Preface |
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lxi | |
Author |
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lxiii | |
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1 Ablation to Axisymmetric Flow |
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1 | (34) |
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1 | (1) |
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2 | (1) |
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1.9 Absolute temperature scale |
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3 | (1) |
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3 | (1) |
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1.12 Acceleration due to gravity |
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4 | (1) |
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1.14 Acceptable noise level |
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4 | (1) |
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1.15 Accuracy vs. precision |
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4 | (1) |
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5 | (1) |
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1.20 Acoustical engineering |
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5 | (1) |
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5 | (1) |
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5 | (1) |
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1.23 Actuator disc theory |
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5 | (1) |
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1.25 Adiabatic efficiency of nozzles |
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6 | (1) |
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1.26 Adiabatic flame temperature |
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6 | (1) |
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6 | (1) |
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6 | (1) |
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1.30 Adverse pressure gradient |
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6 | (1) |
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7 | (1) |
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8 | (1) |
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1.39 Aerodynamic efficiency |
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8 | (1) |
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1.41 Aerodynamic force and moment coefficients |
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9 | (1) |
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1.43 Aerodynamic problems |
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10 | (1) |
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10 | (1) |
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10 | (1) |
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1.46 Aerodynamics in other fields |
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11 | (1) |
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1.47 Aerodynamically untwisted aerofoil |
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11 | (1) |
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11 | (1) |
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11 | (1) |
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1.50 Aerofoil nomenclature |
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12 | (1) |
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12 | (1) |
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1.52 Aerofoils of small aspect ratio |
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13 | (1) |
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13 | (1) |
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13 | (1) |
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13 | (1) |
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14 | (1) |
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14 | (1) |
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1.58 Aerospace engineering |
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14 | (1) |
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14 | (1) |
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14 | (1) |
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15 | (1) |
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15 | (1) |
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15 | (1) |
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16 | (1) |
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16 | (1) |
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16 | (1) |
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16 | (1) |
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16 | (1) |
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16 | (1) |
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1.70 Air traffic control (ATC) |
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17 | (1) |
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17 | (1) |
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1.72 Aircraft classification |
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17 | (1) |
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1.73 Aircraft configurations |
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17 | (1) |
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17 | (1) |
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17 | (1) |
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18 | (1) |
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18 | (1) |
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1.78 Airspeed indicator (ASI) |
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18 | (1) |
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19 | (1) |
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19 | (1) |
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1.81 Alcoholic fermentation |
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19 | (1) |
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20 | (1) |
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1.83 Alfa Laval spray nozzle |
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20 | (1) |
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20 | (1) |
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1.85 Altitude-compensating nozzle |
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20 | (1) |
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1.86 Amagat's law of additive volumes |
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20 | (1) |
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21 | (1) |
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1.88 Ammonia and hydrochloric acid |
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21 | (1) |
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21 | (1) |
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21 | (1) |
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21 | (1) |
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21 | (1) |
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22 | (1) |
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22 | (1) |
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22 | (1) |
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22 | (1) |
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23 | (1) |
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1.98 Angle of attack of helicopter |
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23 | (1) |
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23 | (1) |
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24 | (1) |
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1.101 Annular flow Reynolds number |
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24 | (1) |
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24 | (1) |
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25 | (1) |
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25 | (1) |
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25 | (1) |
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1.106 Archimedes' principle |
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25 | (1) |
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1.107 Area-Mach number relation |
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26 | (1) |
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1.108 Area-velocity relation |
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26 | (1) |
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27 | (1) |
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27 | (1) |
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28 | (1) |
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1.112 Articulated rotor system |
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28 | (1) |
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28 | (1) |
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28 | (1) |
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29 | (1) |
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29 | (1) |
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29 | (1) |
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29 | (1) |
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29 | (1) |
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30 | (1) |
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30 | (1) |
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1.122 Asymmetrical aerofoil |
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30 | (1) |
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30 | (1) |
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1.124 Atmospheric boundary layer |
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31 | (1) |
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1.125 Atmospheric boundary layer thickness |
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31 | (1) |
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1.126 Atmospheric pressure |
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31 | (1) |
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1.127 Atmospheric temperature |
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31 | (1) |
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1.128 Atmospheric turbulence |
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31 | (1) |
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1.129 Audible range of human ear |
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32 | (1) |
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1.130 Automotive cooling system |
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32 | (1) |
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32 | (1) |
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32 | (1) |
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32 | (1) |
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32 | (1) |
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33 | (1) |
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33 | (1) |
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33 | (1) |
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33 | (1) |
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33 | (1) |
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33 | (1) |
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33 | (1) |
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34 | (1) |
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2 Backflow to Bypass Ratio |
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35 | (26) |
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35 | (1) |
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35 | (1) |
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35 | (1) |
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35 | (1) |
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35 | (1) |
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36 | (1) |
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36 | (1) |
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36 | (1) |
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37 | (1) |
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37 | (1) |
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37 | (2) |
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39 | (1) |
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39 | (1) |
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39 | (1) |
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40 | (1) |
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40 | (1) |
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40 | (1) |
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40 | (1) |
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41 | (1) |
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2.20 Basic potential equation for compressible flow |
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41 | (1) |
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2.21 Basic solutions of Laplace's equation |
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42 | (1) |
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42 | (1) |
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2.23 Beckmann thermometer |
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42 | (1) |
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42 | (1) |
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43 | (1) |
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43 | (1) |
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2.27 Bernoulli's equation |
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43 | (1) |
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2.28 Bernoulli's principle |
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44 | (1) |
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44 | (1) |
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44 | (1) |
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2.31 Bimetallic thermometers |
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45 | (1) |
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45 | (1) |
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45 | (1) |
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46 | (1) |
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46 | (1) |
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46 | (1) |
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47 | (1) |
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47 | (1) |
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47 | (1) |
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47 | (1) |
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2.41 Blade element theory |
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47 | (1) |
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47 | (1) |
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48 | (1) |
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2.44 Blasius boundary layer |
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48 | (1) |
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48 | (1) |
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48 | (1) |
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48 | (1) |
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48 | (1) |
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49 | (1) |
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49 | (1) |
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50 | (1) |
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50 | (1) |
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2.53 Blood in the human body |
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50 | (1) |
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50 | (1) |
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50 | (1) |
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2.56 Blowdown tunnel operation |
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51 | (1) |
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51 | (1) |
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51 | (1) |
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51 | (1) |
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51 | (1) |
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52 | (1) |
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52 | (1) |
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2.63 Boiling temperature of water |
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52 | (1) |
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52 | (1) |
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2.65 Boltzmann distribution |
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52 | (1) |
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2.66 Boltzmann equation for entropy |
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52 | (1) |
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53 | (1) |
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53 | (1) |
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2.69 Bose--Einstein statistics |
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53 | (1) |
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53 | (1) |
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53 | (1) |
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54 | (1) |
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54 | (1) |
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2.74 Boundary layer blowing |
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54 | (1) |
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2.75 Boundary layer control |
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55 | (1) |
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2.76 Boundary layer fencing |
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55 | (1) |
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2.77 Boundary layer suction |
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55 | (1) |
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2.78 Boundary layer thickness |
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56 | (1) |
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2.79 Boundary layer tripping |
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56 | (1) |
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56 | (1) |
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57 | (1) |
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57 | (1) |
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58 | (1) |
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58 | (1) |
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2.85 Breathing blunt nose technique |
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58 | (1) |
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58 | (1) |
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58 | (1) |
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59 | (1) |
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59 | (1) |
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59 | (1) |
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2.91 Bucket friction loss coefficient |
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59 | (1) |
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2.92 Buckingham π-theorem |
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59 | (1) |
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59 | (1) |
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59 | (1) |
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60 | (1) |
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60 | (1) |
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60 | (1) |
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3 Calcium to Cylindrical Rectangular Aerofoil |
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61 | (46) |
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61 | (1) |
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61 | (1) |
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61 | (1) |
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3.4 Caloric equations of state |
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61 | (1) |
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62 | (1) |
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62 | (1) |
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3.7 Calorific values of fuel |
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62 | (1) |
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62 | (1) |
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63 | (1) |
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3.10 Canard configuration |
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63 | (1) |
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63 | (1) |
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63 | (1) |
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63 | (1) |
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63 | (1) |
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64 | (1) |
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64 | (1) |
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64 | (1) |
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64 | (1) |
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64 | (1) |
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64 | (1) |
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65 | (1) |
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65 | (1) |
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65 | (1) |
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3.24 Cauchy-Riemann equations |
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65 | (1) |
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66 | (1) |
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66 | (1) |
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66 | (1) |
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3.28 Centre of pressure coefficient |
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67 | (1) |
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67 | (1) |
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67 | (1) |
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67 | (1) |
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67 | (1) |
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68 | (1) |
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68 | (1) |
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68 | (1) |
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68 | (1) |
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68 | (1) |
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3.38 Characteristic decay |
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68 | (1) |
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3.39 Characteristic Mach number |
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69 | (1) |
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69 | (1) |
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69 | (1) |
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69 | (1) |
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3.43 Chemical equilibrium |
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69 | (1) |
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69 | (1) |
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3.45 Chord of an aerofoil |
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70 | (1) |
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70 | (1) |
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70 | (1) |
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70 | (1) |
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3.49 Chromel-alumel thermocouple |
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70 | (1) |
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70 | (1) |
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70 | (1) |
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71 | (1) |
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71 | (1) |
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71 | (1) |
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71 | (1) |
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72 | (1) |
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72 | (1) |
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3.58 Classical hydrodynamics |
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72 | (1) |
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3.59 Classical thermodynamics |
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72 | (1) |
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3.60 Classification of auxiliary lift devices |
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73 | (1) |
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3.61 Classification of hypersonic wind tunnels |
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73 | (1) |
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3.62 Classification of pressure measuring devices |
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73 | (1) |
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3.63 Classification of wind tunnel balance |
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73 | (1) |
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3.64 Clausius statement of the second law is thermodynamics |
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73 | (1) |
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74 | (1) |
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74 | (1) |
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3.67 Closed-circuit tunnel |
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74 | (1) |
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3.68 Closed-throat tunnel |
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74 | (1) |
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74 | (1) |
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74 | (1) |
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75 | (1) |
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75 | (1) |
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75 | (1) |
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75 | (1) |
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76 | (1) |
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76 | (1) |
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76 | (1) |
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3.78 Coefficient of performance |
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76 | (1) |
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3.79 Coefficient of (cubic) thermal expansion |
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77 | (1) |
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3.80 Coefficient of volume expansion |
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77 | (1) |
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77 | (1) |
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77 | (1) |
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77 | (1) |
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77 | (1) |
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3.85 Combined gas-vapour cycle |
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78 | (1) |
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78 | (1) |
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78 | (1) |
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3.88 Combustion temperature of charcoal |
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78 | (1) |
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3.89 Combustion temperature of coal |
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78 | (1) |
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3.90 Combustion temperature of gasoline |
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78 | (1) |
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3.91 Combustion temperature of jet fuel |
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78 | (1) |
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3.92 Combustion temperature of kerosene |
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79 | (1) |
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3.93 Combustion temperature of wood |
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79 | (1) |
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79 | (1) |
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79 | (1) |
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3.96 Components of a wind tunnel |
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79 | (1) |
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79 | (1) |
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80 | (1) |
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80 | (1) |
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80 | (1) |
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81 | (1) |
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81 | (1) |
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3.103 Compressed natural gas |
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81 | (1) |
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3.104 Compressible aerodynamics |
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81 | (1) |
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3.105 Compressible Bernoulli's equation |
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81 | (1) |
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82 | (1) |
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3.107 Compressible flow regimes |
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82 | (1) |
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3.108 Compressible flow pressure coefficient |
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83 | (1) |
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83 | (1) |
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3.110 Compressible subsonic flow |
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84 | (1) |
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84 | (1) |
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3.112 Compressibility factor |
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84 | (1) |
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3.113 Compressibility issues |
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85 | (1) |
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3.114 Compression and expansion corners |
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85 | (1) |
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3.115 Compression ignition engine |
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85 | (1) |
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85 | (1) |
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86 | (1) |
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3.118 Computational fluid dynamics |
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86 | (1) |
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3.119 Concept of lost work |
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86 | (1) |
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86 | (1) |
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86 | (1) |
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3.122 Condensation temperature |
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87 | (1) |
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3.123 Condenser microphones |
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87 | (1) |
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87 | (1) |
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3.125 Conformal transformation |
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87 | (1) |
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87 | (1) |
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87 | (1) |
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3.128 Conservation of energy |
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88 | (1) |
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3.129 Conservation of energy principle |
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88 | (1) |
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3.130 Conservation of entropy principle |
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88 | (1) |
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89 | (1) |
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3.132 Conservation of mass |
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89 | (1) |
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3.133 Conservation of momentum |
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89 | (1) |
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3.134 Conservative system |
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89 | (1) |
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3.135 Constant current anemometer |
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90 | (1) |
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3.136 Constant temperature anemometer |
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90 | (1) |
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3.137 Constant-volume gas thermometer |
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90 | (1) |
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90 | (1) |
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90 | (1) |
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91 | (1) |
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3.141 Continuity equation |
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91 | (1) |
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3.142 Continuous compression |
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92 | (1) |
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92 | (1) |
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3.144 Control of an aircraft |
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93 | (1) |
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93 | (1) |
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93 | (1) |
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93 | (1) |
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93 | (1) |
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93 | (1) |
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94 | (1) |
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3.151 Convective acceleration |
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94 | (1) |
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3.152 Convective heat transfer |
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94 | (1) |
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3.153 Convective beat transfer coefficient |
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94 | (1) |
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3.154 Convective Mach number |
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95 | (1) |
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3.155 Convective mass transfer |
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95 | (1) |
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95 | (1) |
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3.157 Convergent-divergent nozzle |
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95 | (1) |
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96 | (1) |
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96 | (1) |
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96 | (1) |
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3.161 Copper-constantan thermocouple |
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96 | (1) |
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96 | (1) |
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96 | (1) |
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97 | (1) |
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3.165 Correctly expanded operation |
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97 | (1) |
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97 | (1) |
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98 | (1) |
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98 | (1) |
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98 | (1) |
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99 | (1) |
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3.171 Critical angle of attack |
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99 | (1) |
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3.172 Critical circulation |
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99 | (1) |
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3.173 Critical Mach number |
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99 | (1) |
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99 | (1) |
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99 | (1) |
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99 | (1) |
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3.177 Critical properties |
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100 | (1) |
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3.178 Critical Reynolds number |
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100 | (1) |
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3.179 Critical Reynolds number for flat plate |
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100 | (1) |
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3.180 Critical Reynolds number for open channel flow |
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100 | (1) |
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3.181 Critical Reynolds number for pipe flow |
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100 | (1) |
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100 | (1) |
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3.183 Critical temperature |
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101 | (1) |
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101 | (1) |
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101 | (1) |
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101 | (1) |
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101 | (1) |
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101 | (1) |
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102 | (1) |
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102 | (1) |
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102 | (1) |
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3.192 Cryogenic fluid properties |
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102 | (1) |
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3.193 Cryogenic propellants |
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102 | (1) |
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3.194 Cryogenic temperature |
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102 | (1) |
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103 | (1) |
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103 | (1) |
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103 | (1) |
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103 | (1) |
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104 | (1) |
|
|
104 | (1) |
|
|
104 | (1) |
|
3.202 Cyclonic depression |
|
|
105 | (1) |
|
3.203 Cylindrical rectangular aerofoil |
|
|
105 | (2) |
|
4 d'Alembert's Paradox to Dynamics |
|
|
107 | (20) |
|
|
107 | (1) |
|
4.2 Dalton's law of additive pressures |
|
|
107 | (1) |
|
4.3 Dalton's law of partial pressures |
|
|
107 | (1) |
|
4.4 Darcy friction factor |
|
|
107 | (1) |
|
|
108 | (1) |
|
|
108 | (1) |
|
4.7 Darcy--Weisbach equation |
|
|
108 | (1) |
|
|
108 | (1) |
|
|
109 | (1) |
|
|
109 | (1) |
|
|
109 | (1) |
|
|
109 | (1) |
|
|
110 | (1) |
|
|
110 | (1) |
|
|
110 | (1) |
|
|
110 | (1) |
|
4.17 Density of pure water |
|
|
111 | (1) |
|
|
111 | (1) |
|
|
111 | (1) |
|
|
111 | (1) |
|
|
112 | (1) |
|
|
112 | (1) |
|
4.23 Dew-point temperature |
|
|
112 | (1) |
|
4.24 Dial-type pressure gauge |
|
|
112 | (1) |
|
4.25 Diaphragm pressure gauges |
|
|
112 | (1) |
|
|
113 | (1) |
|
4.27 Differences between the jet and piston engine aircraft |
|
|
113 | (1) |
|
4.28 Differential aileron |
|
|
114 | (1) |
|
4.29 Differential analysis |
|
|
114 | (1) |
|
4.30 Different types of winglets |
|
|
114 | (1) |
|
|
115 | (1) |
|
|
115 | (1) |
|
|
115 | (1) |
|
|
115 | (1) |
|
|
115 | (1) |
|
|
116 | (1) |
|
|
116 | (1) |
|
4.38 Dimensional analysis |
|
|
116 | (1) |
|
4.39 Dimensionless groups |
|
|
116 | (1) |
|
4.40 Dimensions and units |
|
|
116 | (1) |
|
4.41 Dimensionless velocity |
|
|
117 | (1) |
|
4.42 Direct Simulation Monte Carlo (DSMC) |
|
|
117 | (1) |
|
4.43 Directional stability |
|
|
117 | (1) |
|
|
117 | (1) |
|
|
118 | (1) |
|
4.46 Discharge coefficient |
|
|
118 | (1) |
|
|
118 | (1) |
|
|
119 | (1) |
|
4.49 Displacement thickness |
|
|
119 | (1) |
|
|
119 | (1) |
|
|
120 | (1) |
|
|
120 | (1) |
|
|
120 | (1) |
|
|
120 | (1) |
|
|
120 | (1) |
|
|
121 | (1) |
|
|
121 | (1) |
|
4.58 Downwash consequences |
|
|
121 | (1) |
|
|
121 | (1) |
|
|
122 | (1) |
|
|
122 | (1) |
|
4.62 Drag-divergence Mach number |
|
|
123 | (1) |
|
|
123 | (1) |
|
|
123 | (1) |
|
|
123 | (1) |
|
|
123 | (1) |
|
|
124 | (1) |
|
|
124 | (1) |
|
|
124 | (1) |
|
|
124 | (1) |
|
|
124 | (1) |
|
|
124 | (1) |
|
|
124 | (1) |
|
|
125 | (1) |
|
|
125 | (1) |
|
|
125 | (1) |
|
|
126 | (1) |
|
|
126 | (1) |
|
|
126 | (1) |
|
4.80 Dynamic pressure gauges |
|
|
126 | (1) |
|
|
126 | (1) |
|
5 Eckert Number to Extratropical Cyclone |
|
|
127 | (18) |
|
|
127 | (1) |
|
|
127 | (1) |
|
|
127 | (1) |
|
|
127 | (1) |
|
5.5 Eddy viscosity turbulence models |
|
|
128 | (1) |
|
5.6 Effective angle of attack |
|
|
128 | (1) |
|
|
128 | (1) |
|
|
128 | (1) |
|
5.9 Effects of the Earth's rotation |
|
|
128 | (1) |
|
5.10 Effects of the second throat |
|
|
129 | (1) |
|
5.11 Efficiency of turbines |
|
|
129 | (1) |
|
|
129 | (1) |
|
5.13 Ekman boundary layer |
|
|
129 | (1) |
|
|
130 | (1) |
|
|
130 | (1) |
|
|
130 | (1) |
|
|
130 | (1) |
|
|
130 | (1) |
|
|
130 | (1) |
|
|
131 | (1) |
|
|
131 | (1) |
|
5.22 Endothermic reaction |
|
|
131 | (1) |
|
|
131 | (1) |
|
5.24 Endurance of jet engine |
|
|
132 | (1) |
|
5.25 Energy efficiency rating |
|
|
132 | (1) |
|
|
132 | (1) |
|
|
132 | (1) |
|
|
132 | (1) |
|
|
132 | (1) |
|
|
133 | (1) |
|
|
133 | (1) |
|
5.32 Enthalpy of combustion |
|
|
133 | (1) |
|
5.33 Enthalpy of formation |
|
|
133 | (1) |
|
5.34 Enthalpy of reaction |
|
|
133 | (1) |
|
5.35 Enthalpy of vapourisation |
|
|
134 | (1) |
|
|
134 | (1) |
|
|
134 | (1) |
|
|
134 | (1) |
|
|
135 | (1) |
|
|
135 | (1) |
|
|
135 | (1) |
|
|
135 | (1) |
|
|
135 | (1) |
|
|
135 | (1) |
|
|
135 | (1) |
|
|
136 | (1) |
|
|
136 | (1) |
|
5.48 Equilibrium Mach number |
|
|
136 | (1) |
|
5.49 Equilibrium speed of sound |
|
|
136 | (1) |
|
5.50 Equipartition of energy |
|
|
136 | (1) |
|
|
137 | (1) |
|
5.52 Equivalent airspeed (EAS) |
|
|
137 | (1) |
|
|
137 | (1) |
|
|
137 | (1) |
|
5.55 Escape velocity of Earth |
|
|
137 | (1) |
|
5.56 Euler's acceleration formula |
|
|
137 | (1) |
|
|
138 | (1) |
|
5.58 Eulerian description |
|
|
138 | (1) |
|
|
139 | (1) |
|
|
139 | (1) |
|
|
139 | (1) |
|
|
139 | (1) |
|
|
140 | (1) |
|
|
140 | (1) |
|
|
140 | (1) |
|
5.66 Expansion levels of jets |
|
|
140 | (1) |
|
|
141 | (1) |
|
|
141 | (1) |
|
|
141 | (1) |
|
5.70 Experimental accuracy |
|
|
141 | (1) |
|
|
141 | (1) |
|
5.72 Experimental mean pitch |
|
|
142 | (1) |
|
|
142 | (1) |
|
5.74 Extensive properties |
|
|
142 | (1) |
|
5.75 External aerodynamics |
|
|
142 | (1) |
|
|
142 | (1) |
|
|
142 | (1) |
|
5.78 Externally reversible process |
|
|
143 | (1) |
|
5.79 Extratropical cyclone |
|
|
143 | (2) |
|
6 Factors Influencing Pitot-Static Tube Performance to Fusion Pyrometers |
|
|
145 | (28) |
|
6.1 Factors influencing pitot-static tube performance |
|
|
145 | (1) |
|
|
145 | (1) |
|
|
145 | (1) |
|
6.4 Favourable pressure gradient |
|
|
145 | (1) |
|
|
145 | (1) |
|
|
146 | (1) |
|
|
146 | (1) |
|
|
146 | (1) |
|
|
146 | (1) |
|
6.10 Fermi-Dirac statistics |
|
|
146 | (1) |
|
|
146 | (1) |
|
|
147 | (1) |
|
|
147 | (1) |
|
|
147 | (1) |
|
|
148 | (1) |
|
|
148 | (1) |
|
|
148 | (1) |
|
|
149 | (1) |
|
6.19 Finite or three-dimensional wing |
|
|
149 | (1) |
|
|
149 | (1) |
|
6.21 First law of thermodynamics |
|
|
150 | (1) |
|
|
150 | (1) |
|
6.23 Five-hole yaw probes |
|
|
150 | (1) |
|
|
150 | (1) |
|
|
150 | (1) |
|
|
150 | (1) |
|
|
151 | (1) |
|
|
151 | (1) |
|
6.29 Flap effect on aerodynamic centre |
|
|
152 | (1) |
|
|
152 | (1) |
|
|
152 | (1) |
|
|
152 | (1) |
|
|
152 | (1) |
|
|
153 | (1) |
|
6.35 Flattening out flight |
|
|
153 | (1) |
|
|
153 | (1) |
|
|
153 | (1) |
|
|
153 | (1) |
|
6.39 Floating element method |
|
|
153 | (1) |
|
|
154 | (1) |
|
|
154 | (1) |
|
|
154 | (1) |
|
6.43 Flow deflection angle |
|
|
155 | (1) |
|
6.44 Flow development length |
|
|
155 | (1) |
|
6.45 Flow-induced vibration |
|
|
155 | (1) |
|
|
155 | (1) |
|
|
155 | (1) |
|
6.48 Flow of multicomponent mixtures |
|
|
155 | (1) |
|
6.49 Flow past a flat plate |
|
|
156 | (1) |
|
|
156 | (1) |
|
|
156 | (1) |
|
|
157 | (1) |
|
|
157 | (1) |
|
|
157 | (1) |
|
|
157 | (1) |
|
|
157 | (1) |
|
|
157 | (1) |
|
6.58 Fluid mechanics of perfect fluids |
|
|
158 | (1) |
|
6.59 Fluid mechanics of real fluids |
|
|
158 | (1) |
|
|
158 | (1) |
|
|
158 | (1) |
|
6.62 Fluids and the continuum |
|
|
158 | (1) |
|
6.63 Fluid-jet anemometer |
|
|
158 | (1) |
|
|
159 | (1) |
|
|
159 | (1) |
|
6.66 Fluorinated greenhouse gases |
|
|
160 | (1) |
|
|
160 | (1) |
|
|
161 | (1) |
|
|
161 | (1) |
|
|
161 | (1) |
|
|
161 | (1) |
|
6.72 Force and moment of a flying machine |
|
|
161 | (1) |
|
|
161 | (1) |
|
|
162 | (1) |
|
|
163 | (1) |
|
|
164 | (1) |
|
|
164 | (1) |
|
|
164 | (1) |
|
6.79 Fourier's law of heat conduction |
|
|
165 | (1) |
|
|
165 | (1) |
|
|
166 | (1) |
|
|
166 | (1) |
|
|
166 | (1) |
|
|
167 | (1) |
|
|
167 | (1) |
|
|
167 | (1) |
|
|
167 | (1) |
|
|
168 | (1) |
|
6.89 Friction coefficient |
|
|
168 | (1) |
|
|
168 | (1) |
|
|
168 | (1) |
|
|
168 | (1) |
|
|
168 | (1) |
|
|
169 | (1) |
|
|
169 | (1) |
|
|
169 | (1) |
|
|
169 | (1) |
|
|
170 | (1) |
|
|
170 | (1) |
|
6.100 Fully developed flow |
|
|
170 | (1) |
|
6.101 Fully developed pipe flow |
|
|
170 | (1) |
|
6.102 Fully developed region |
|
|
170 | (1) |
|
|
170 | (1) |
|
|
170 | (1) |
|
|
171 | (1) |
|
|
171 | (2) |
|
7 Gas to Gyroscopic Effect |
|
|
173 | (14) |
|
|
173 | (1) |
|
|
173 | (1) |
|
|
173 | (1) |
|
7.4 Gas dynamics divisions |
|
|
174 | (1) |
|
|
174 | (1) |
|
|
174 | (1) |
|
7.7 Gas refrigeration cycle |
|
|
174 | (1) |
|
|
175 | (1) |
|
|
175 | (1) |
|
|
175 | (1) |
|
7.11 Gasoline boiling point |
|
|
175 | (1) |
|
|
175 | (1) |
|
|
175 | (1) |
|
|
176 | (1) |
|
7.15 Geometrical angle of attack |
|
|
176 | (1) |
|
7.16 Geometrical incidence |
|
|
176 | (1) |
|
|
176 | (1) |
|
|
176 | (1) |
|
7.19 Geostationary satellite |
|
|
176 | (1) |
|
|
177 | (1) |
|
|
177 | (1) |
|
|
177 | (1) |
|
|
177 | (1) |
|
|
177 | (1) |
|
|
177 | (1) |
|
|
178 | (1) |
|
|
178 | (1) |
|
7.28 Gladstone-Dale empirical equation |
|
|
179 | (1) |
|
|
179 | (1) |
|
|
179 | (1) |
|
|
180 | (1) |
|
|
180 | (1) |
|
|
180 | (1) |
|
|
180 | (1) |
|
|
180 | (1) |
|
|
180 | (1) |
|
|
181 | (1) |
|
|
181 | (1) |
|
7.39 Gradually varied flow |
|
|
181 | (1) |
|
|
181 | (1) |
|
|
181 | (1) |
|
|
181 | (1) |
|
|
182 | (1) |
|
|
182 | (1) |
|
|
182 | (1) |
|
|
183 | (1) |
|
|
183 | (1) |
|
|
183 | (1) |
|
|
183 | (1) |
|
|
183 | (1) |
|
|
183 | (1) |
|
|
184 | (1) |
|
|
184 | (1) |
|
|
184 | (1) |
|
|
184 | (1) |
|
|
184 | (1) |
|
|
185 | (1) |
|
|
185 | (2) |
|
|
187 | (20) |
|
|
187 | (1) |
|
|
187 | (1) |
|
|
187 | (1) |
|
|
187 | (1) |
|
|
187 | (1) |
|
8.6 Hartmann--Sprenger tube |
|
|
188 | (1) |
|
|
188 | (1) |
|
|
188 | (1) |
|
|
188 | (1) |
|
|
189 | (1) |
|
|
189 | (1) |
|
|
189 | (1) |
|
|
189 | (1) |
|
|
189 | (1) |
|
8.15 Heat transfer from rockets |
|
|
190 | (1) |
|
|
190 | (1) |
|
|
190 | (1) |
|
|
190 | (1) |
|
8.19 Hele--Shaw apparatus |
|
|
190 | (1) |
|
|
191 | (1) |
|
|
191 | (1) |
|
8.22 Helicopter configurations |
|
|
192 | (1) |
|
|
192 | (1) |
|
|
192 | (1) |
|
8.25 Helmholtz's theorems |
|
|
193 | (1) |
|
8.26 Heterogeneous system |
|
|
193 | (1) |
|
|
193 | (1) |
|
8.28 High-enthalpy facilities |
|
|
193 | (1) |
|
|
193 | (1) |
|
|
194 | (1) |
|
|
194 | (1) |
|
|
194 | (1) |
|
|
194 | (1) |
|
8.34 High-speed wind tunnel |
|
|
194 | (1) |
|
|
194 | (1) |
|
8.36 Highly underexpanded jet |
|
|
195 | (1) |
|
8.37 Hohmann minimum-energy trajectory |
|
|
195 | (1) |
|
|
195 | (1) |
|
|
195 | (1) |
|
|
195 | (1) |
|
|
196 | (1) |
|
|
196 | (1) |
|
|
196 | (1) |
|
|
197 | (1) |
|
|
197 | (1) |
|
8.46 Hot-wire anemometer working principle |
|
|
197 | (1) |
|
|
198 | (1) |
|
|
198 | (1) |
|
|
198 | (1) |
|
|
198 | (1) |
|
|
198 | (1) |
|
8.52 Human body temperature |
|
|
199 | (1) |
|
8.53 Human breathing rate |
|
|
199 | (1) |
|
8.54 Human hearing limits |
|
|
199 | (1) |
|
|
199 | (1) |
|
|
199 | (1) |
|
|
199 | (1) |
|
|
200 | (1) |
|
|
200 | (1) |
|
8.60 Hydraulic analogy theory |
|
|
201 | (1) |
|
|
201 | (1) |
|
8.62 Hydraulic efficiency |
|
|
201 | (1) |
|
8.63 Hydraulic grade line (HGL) |
|
|
201 | (1) |
|
|
201 | (1) |
|
|
201 | (1) |
|
|
202 | (1) |
|
|
202 | (1) |
|
8.68 Hydraulic mean depth |
|
|
202 | (1) |
|
|
202 | (1) |
|
|
203 | (1) |
|
|
203 | (1) |
|
|
203 | (1) |
|
|
203 | (1) |
|
|
203 | (1) |
|
|
203 | (1) |
|
|
204 | (1) |
|
|
204 | (1) |
|
|
204 | (1) |
|
|
204 | (1) |
|
8.80 Hydrostatic pressure distribution |
|
|
204 | (1) |
|
|
204 | (1) |
|
8.82 Hypersonic experimental facilities |
|
|
204 | (1) |
|
|
205 | (1) |
|
|
205 | (1) |
|
8.85 Hypersonic similarity parameter |
|
|
205 | (1) |
|
|
205 | (1) |
|
8.87 Hypervelocity facilities |
|
|
205 | (1) |
|
|
206 | (1) |
|
|
206 | (1) |
|
|
207 | (18) |
|
|
207 | (1) |
|
|
207 | (1) |
|
|
207 | (1) |
|
|
207 | (1) |
|
|
208 | (1) |
|
|
208 | (1) |
|
|
208 | (1) |
|
|
208 | (1) |
|
|
208 | (1) |
|
|
209 | (1) |
|
|
209 | (1) |
|
|
209 | (1) |
|
|
210 | (1) |
|
9.14 Incompressible aerodynamics |
|
|
210 | (1) |
|
|
210 | (1) |
|
|
211 | (1) |
|
9.17 Incompressible substance |
|
|
211 | (1) |
|
9.18 Increase-in-entropy principle |
|
|
211 | (1) |
|
9.19 Indicated airspeed (IAS) |
|
|
211 | (1) |
|
|
212 | (1) |
|
|
212 | (1) |
|
|
212 | (1) |
|
|
212 | (1) |
|
9.24 Induced velocity field |
|
|
212 | (1) |
|
|
213 | (1) |
|
|
213 | (1) |
|
|
213 | (1) |
|
|
213 | (1) |
|
|
213 | (1) |
|
9.30 Infrared thermography |
|
|
213 | (1) |
|
|
213 | (1) |
|
|
214 | (1) |
|
|
214 | (1) |
|
9.34 Instrument landing system (ILS) |
|
|
214 | (1) |
|
|
214 | (1) |
|
|
214 | (1) |
|
9.37 Intensive properties |
|
|
215 | (1) |
|
|
215 | (1) |
|
|
215 | (1) |
|
|
215 | (1) |
|
|
215 | (1) |
|
9.42 Internal aerodynamics |
|
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215 | (1) |
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216 | (1) |
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216 | (1) |
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216 | (1) |
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9.46 Internally reversible process |
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217 | (1) |
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9.47 International space station |
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217 | (1) |
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9.48 International Standard Atmosphere |
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217 | (1) |
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9.49 Intersection of shocks of the same family |
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218 | (1) |
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218 | (1) |
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218 | (1) |
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218 | (1) |
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219 | (1) |
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219 | (1) |
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220 | (1) |
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220 | (1) |
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9.57 Irreversible process |
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220 | (1) |
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220 | (1) |
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220 | (1) |
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9.60 Irrigation sprinkler |
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220 | (1) |
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220 | (1) |
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9.62 Isentropic compression |
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221 | (1) |
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221 | (1) |
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221 | (1) |
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222 | (1) |
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9.66 Isentropic process relation |
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222 | (1) |
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9.67 Isentropic relations |
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222 | (1) |
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9.68 Isentropic stagnation state |
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223 | (1) |
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223 | (1) |
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223 | (1) |
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223 | (1) |
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223 | (1) |
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223 | (1) |
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224 | (1) |
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224 | (1) |
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10 Jelly to Joule--Thomson Effect |
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225 | (8) |
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225 | (1) |
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225 | (1) |
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225 | (1) |
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225 | (1) |
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226 | (1) |
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10.6 Jet engine combustor |
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226 | (1) |
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10.7 Jet engine components |
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227 | (1) |
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10.8 Jet engine compressor |
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227 | (1) |
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227 | (1) |
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227 | (1) |
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228 | (1) |
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228 | (1) |
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228 | (1) |
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10.14 Jet fuel composition |
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229 | (1) |
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229 | (1) |
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229 | (1) |
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229 | (1) |
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10.18 Jet-propulsion cycle |
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229 | (1) |
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230 | (1) |
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230 | (1) |
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10.21 Joukowski hypothesis |
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230 | (1) |
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230 | (1) |
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10.23 Joule--Thomson coefficient |
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230 | (1) |
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10.24 Joule--Thomson effect |
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231 | (2) |
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11 Kaplan Turbine to Kutta--Joukowski Transformation |
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233 | (10) |
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233 | (1) |
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11.2 Karman vortex street |
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233 | (1) |
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233 | (1) |
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11.4 Kelvin's circulation theorem |
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233 | (1) |
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11.5 Kelvin-Planck statement |
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234 | (1) |
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11.6 k-epsilon turbulence model |
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235 | (1) |
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11.7 Kepler's laws of planetary motion |
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235 | (1) |
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235 | (1) |
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11.9 Kerosene boiling point |
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235 | (1) |
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235 | (1) |
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11.11 Kerosene smoke generator |
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236 | (1) |
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236 | (1) |
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11.13 Kinematics of fluids |
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236 | (1) |
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11.14 Kinematics of fluid flow |
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237 | (1) |
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11.15 Kinematic viscosity coefficient |
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237 | (1) |
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237 | (1) |
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237 | (1) |
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11.18 Kinetic energy of gas |
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238 | (1) |
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11.19 Kinetic energy thickness |
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238 | (1) |
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11.20 Kinetic theory of gases |
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238 | (1) |
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11.21 Kinetic theory equivalent of the perfect gas state equation |
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238 | (1) |
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238 | (1) |
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238 | (1) |
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239 | (1) |
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239 | (1) |
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239 | (1) |
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239 | (1) |
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239 | (1) |
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11.29 Kutta--Zhukovsky lift theorem |
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|
240 | (1) |
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11.30 Kutta--Joukowski transformation |
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241 | (2) |
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243 | (22) |
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243 | (1) |
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243 | (1) |
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243 | (1) |
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243 | (1) |
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12.5 Lagrangian description |
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243 | (1) |
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244 | (1) |
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244 | (1) |
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244 | (1) |
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12.9 Laminar separation bubble |
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245 | (1) |
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245 | (1) |
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12.11 Lancaster--Prandtl lifting-line theory |
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245 | (1) |
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245 | (1) |
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246 | (1) |
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246 | (1) |
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246 | (1) |
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|
247 | (1) |
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12.17 Large eddy simulation |
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|
247 | (1) |
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247 | (1) |
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12.19 Laser Doppler anemometer |
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|
247 | (1) |
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247 | (1) |
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247 | (1) |
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12.22 Latent heat of fusion |
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|
248 | (1) |
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12.23 Latent heat of vaporisation |
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|
248 | (1) |
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12.24 Lateral acceleration |
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|
248 | (1) |
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248 | (1) |
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248 | (1) |
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248 | (1) |
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248 | (1) |
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249 | (1) |
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12.30 Law of conservation of energy |
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|
249 | (1) |
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12.31 Law of dimensional homogeneity |
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|
250 | (1) |
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250 | (1) |
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12.33 Law of intermediate metals |
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250 | (1) |
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250 | (1) |
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250 | (1) |
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12.36 Layers of the Earth |
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250 | (1) |
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250 | (1) |
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251 | (1) |
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251 | (1) |
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251 | (1) |
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12.41 Leading-edge radius |
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251 | (1) |
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252 | (1) |
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252 | (1) |
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252 | (1) |
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|
252 | (1) |
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|
253 | (1) |
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253 | (1) |
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253 | (1) |
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253 | (1) |
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253 | (1) |
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254 | (1) |
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12.52 Lifting-line theory |
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|
254 | (1) |
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12.53 Lifting surface theory |
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|
254 | (1) |
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|
254 | (1) |
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254 | (1) |
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|
255 | (1) |
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255 | (1) |
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12.58 Limitations on air as a perfect gas |
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|
255 | (1) |
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12.59 Limitations of hot-wire anemometer |
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|
256 | (1) |
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12.60 Limitations of hydraulic analogy |
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|
256 | (1) |
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256 | (1) |
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|
257 | (1) |
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12.63 Linear variable differential transformer (LVDT) |
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|
257 | (1) |
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|
257 | (1) |
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|
257 | (1) |
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|
258 | (1) |
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|
258 | (1) |
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|
258 | (1) |
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12.69 Liquid-propellant rocket |
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|
258 | (1) |
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|
258 | (1) |
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|
258 | (1) |
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12.72 Liquefied petroleum gas |
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|
259 | (1) |
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|
259 | (1) |
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|
259 | (1) |
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12.75 Lobed-impeller meter |
|
|
259 | (1) |
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12.76 Local chemical equilibrium |
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|
260 | (1) |
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12.77 Local rate of change |
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|
260 | (1) |
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12.78 Local thermodynamic equilibrium |
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|
260 | (1) |
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|
260 | (1) |
|
12.80 Longitudinal dihedral |
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|
260 | (1) |
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12.81 Longitudinal stability |
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|
260 | (1) |
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|
261 | (1) |
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|
261 | (1) |
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|
261 | (1) |
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|
261 | (1) |
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|
261 | (1) |
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261 | (1) |
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12.88 Low-speed wind tunnels |
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|
262 | (1) |
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|
262 | (1) |
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12.90 Lower critical Reynolds number |
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|
262 | (1) |
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|
262 | (1) |
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|
262 | (1) |
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|
262 | (1) |
|
12.94 Ludwieg tube advantages |
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|
263 | (1) |
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|
263 | (1) |
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|
263 | (2) |
|
13 Mach to Munk's Theorem of Stagger |
|
|
265 | (24) |
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|
265 | (1) |
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|
265 | (1) |
|
13.3 Mach angle - Mach number relation |
|
|
265 | (1) |
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|
266 | (1) |
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|
266 | (1) |
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|
267 | (1) |
|
13.7 Mach number independence principle |
|
|
267 | (1) |
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|
268 | (1) |
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|
268 | (1) |
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|
268 | (1) |
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|
268 | (1) |
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|
269 | (1) |
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|
269 | (1) |
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|
269 | (1) |
|
13.15 Magnetofluidmechanics |
|
|
269 | (1) |
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|
269 | (1) |
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|
270 | (1) |
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|
270 | (1) |
|
13.19 Manoeuvres of an aircraft |
|
|
270 | (1) |
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|
270 | (1) |
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|
271 | (1) |
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|
271 | (1) |
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|
271 | (1) |
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|
271 | (1) |
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|
272 | (1) |
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|
272 | (1) |
|
13.27 Mass-motion velocity |
|
|
272 | (1) |
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|
272 | (1) |
|
13.29 Material derivative |
|
|
272 | (1) |
|
13.30 Material description |
|
|
272 | (1) |
|
|
273 | (1) |
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|
273 | (1) |
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|
273 | (1) |
|
13.34 Maxwell's definition of viscosity |
|
|
273 | (1) |
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|
273 | (1) |
|
13.36 Maxwell-Boltzmann statistics |
|
|
274 | (1) |
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|
274 | (1) |
|
13.38 Mean aerodynamic chord |
|
|
274 | (1) |
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|
274 | (1) |
|
13.40 Mean effective pressure |
|
|
275 | (1) |
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|
275 | (1) |
|
13.42 Mean free path length |
|
|
275 | (1) |
|
13.43 Measuring principle of the liquid manometer |
|
|
275 | (1) |
|
13.44 Mechanical equilibrium |
|
|
275 | (1) |
|
13.45 Mechanics of fluids |
|
|
275 | (1) |
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|
276 | (1) |
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|
276 | (1) |
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|
277 | (1) |
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|
277 | (1) |
|
13.50 Melting point of water |
|
|
277 | (1) |
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|
277 | (1) |
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|
277 | (1) |
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|
278 | (1) |
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|
278 | (1) |
|
13.55 Method of characteristics |
|
|
278 | (1) |
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|
278 | (1) |
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|
279 | (1) |
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|
279 | (1) |
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|
279 | (1) |
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|
280 | (1) |
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|
280 | (1) |
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|
280 | (1) |
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|
280 | (1) |
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|
280 | (1) |
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|
281 | (1) |
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|
281 | (1) |
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|
281 | (1) |
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|
282 | (1) |
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|
282 | (1) |
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|
282 | (1) |
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|
282 | (1) |
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|
282 | (1) |
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|
282 | (1) |
|
13.74 Moisture and humidity |
|
|
282 | (1) |
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|
283 | (1) |
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|
283 | (1) |
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|
283 | (1) |
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|
283 | (1) |
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|
283 | (1) |
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|
283 | (1) |
|
13.81 Molecular gas dynamics |
|
|
284 | (1) |
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|
284 | (1) |
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|
284 | (1) |
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|
284 | (1) |
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|
284 | (2) |
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|
286 | (1) |
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|
286 | (1) |
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|
286 | (1) |
|
|
286 | (1) |
|
13.90 Monte Carlo methods |
|
|
286 | (1) |
|
|
287 | (1) |
|
13.92 Most probable macrostate |
|
|
287 | (1) |
|
13.93 Movement of centre of pressure |
|
|
288 | (1) |
|
13.94 Moving boundary work |
|
|
288 | (1) |
|
|
288 | (1) |
|
13.96 Multiple slotted flaps |
|
|
288 | (1) |
|
13.97 Munk's theorem of stagger |
|
|
288 | (1) |
|
14 Natural Convection to Nusselt Number |
|
|
289 | (12) |
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|
289 | (1) |
|
|
289 | (1) |
|
14.3 Nature of high-enthalpy flows |
|
|
290 | (1) |
|
14.4 Navier-Stokes equations |
|
|
290 | (1) |
|
|
291 | (1) |
|
14.6 Negative angle of attack |
|
|
291 | (1) |
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|
291 | (1) |
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|
291 | (1) |
|
|
292 | (1) |
|
14.10 Newtonian flow model |
|
|
292 | (1) |
|
14.11 Newton's law of gravitation |
|
|
292 | (1) |
|
14.12 Newton's laws of motion |
|
|
292 | (1) |
|
14.13 Newton's law of viscosity |
|
|
292 | (1) |
|
14.14 Newton's second law |
|
|
293 | (1) |
|
|
293 | (1) |
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|
293 | (1) |
|
|
293 | (1) |
|
|
293 | (1) |
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|
293 | (1) |
|
|
294 | (1) |
|
|
294 | (1) |
|
|
294 | (1) |
|
|
294 | (1) |
|
14.24 Noise pollution effects |
|
|
294 | (1) |
|
14.25 Noise of supersonic jet |
|
|
294 | (1) |
|
14.26 Non-chemical rocket |
|
|
295 | (1) |
|
14.27 Non-conservative system |
|
|
295 | (1) |
|
14.28 Non-Newtonian fluid |
|
|
295 | (1) |
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|
295 | (1) |
|
|
296 | (1) |
|
|
296 | (1) |
|
|
296 | (1) |
|
14.33 Normal shock relations |
|
|
296 | (1) |
|
14.34 Normal shock tables |
|
|
297 | (1) |
|
|
297 | (1) |
|
|
298 | (1) |
|
14.37 Nozzle discharge coefficient |
|
|
299 | (1) |
|
|
299 | (1) |
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|
299 | (2) |
|
|
301 | (10) |
|
|
301 | (1) |
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|
301 | (1) |
|
15.3 Obstruction or constriction meters |
|
|
302 | (1) |
|
|
302 | (1) |
|
15.5 Ocean and sea difference |
|
|
302 | (1) |
|
|
303 | (1) |
|
|
303 | (1) |
|
|
303 | (1) |
|
|
304 | (1) |
|
15.10 One-dimensional flow |
|
|
304 | (1) |
|
|
304 | (1) |
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|
304 | (1) |
|
15.13 Open-circuit tunnels |
|
|
304 | (1) |
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|
304 | (1) |
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|
305 | (1) |
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|
305 | (1) |
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|
305 | (1) |
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|
305 | (1) |
|
|
306 | (1) |
|
15.20 Optical-type pressure transducer |
|
|
306 | (1) |
|
|
307 | (1) |
|
|
307 | (1) |
|
|
307 | (1) |
|
|
307 | (1) |
|
15.25 Oscillatory motion types |
|
|
308 | (1) |
|
|
308 | (1) |
|
|
308 | (1) |
|
15.28 Oswald efficiency number |
|
|
308 | (1) |
|
15.29 Oswald wing efficiency |
|
|
308 | (1) |
|
|
309 | (1) |
|
|
309 | (1) |
|
15.32 Overall pressure ratio |
|
|
309 | (1) |
|
15.33 Overall propulsive efficiency |
|
|
309 | (1) |
|
15.34 Overexpanded nozzle |
|
|
309 | (1) |
|
|
309 | (1) |
|
|
310 | (1) |
|
|
310 | (1) |
|
|
310 | (1) |
|
|
310 | (1) |
|
16 Pacific Ocean to Pyrometers |
|
|
311 | (34) |
|
|
311 | (1) |
|
|
311 | (1) |
|
|
311 | (1) |
|
|
311 | (1) |
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|
312 | (1) |
|
|
312 | (1) |
|
|
312 | (1) |
|
|
312 | (1) |
|
16.9 Partially filled flow |
|
|
313 | (1) |
|
|
313 | (1) |
|
|
313 | (1) |
|
16.12 Particle image velocimetry (PIV) |
|
|
313 | (1) |
|
|
314 | (1) |
|
|
314 | (1) |
|
|
314 | (1) |
|
|
314 | (1) |
|
|
315 | (1) |
|
|
315 | (1) |
|
|
315 | (1) |
|
16.20 Pelton wheel turbine |
|
|
316 | (1) |
|
|
316 | (1) |
|
|
316 | (1) |
|
|
317 | (1) |
|
16.24 Perfect gas equation of state |
|
|
317 | (1) |
|
|
317 | (1) |
|
16.26 Performance of actual nozzles |
|
|
318 | (1) |
|
|
318 | (1) |
|
16.28 Peripheral-velocity factor |
|
|
318 | (1) |
|
|
318 | (1) |
|
16.30 Perpetual-motion machine |
|
|
318 | (1) |
|
16.31 Perpetual-motion machine of the first kind (PMM1) |
|
|
318 | (1) |
|
16.32 Perpetual-motion machine of the second kind (PMM2) |
|
|
319 | (1) |
|
|
319 | (1) |
|
|
319 | (1) |
|
|
319 | (1) |
|
|
319 | (1) |
|
16.37 Phases of a pure substance |
|
|
319 | (1) |
|
|
319 | (1) |
|
|
320 | (1) |
|
|
320 | (1) |
|
|
320 | (1) |
|
16.42 Physical properties of fluids |
|
|
320 | (1) |
|
|
320 | (1) |
|
|
321 | (1) |
|
|
321 | (1) |
|
|
321 | (1) |
|
16.47 Pitch of a propeller |
|
|
321 | (1) |
|
|
321 | (1) |
|
|
322 | (1) |
|
|
322 | (1) |
|
|
322 | (1) |
|
|
323 | (1) |
|
16.53 Pitot-static tube characteristics |
|
|
323 | (1) |
|
16.54 Pitot-static tube limitations |
|
|
323 | (1) |
|
16.55 PIV seeding particles |
|
|
324 | (1) |
|
|
324 | (1) |
|
|
324 | (1) |
|
|
324 | (1) |
|
|
325 | (1) |
|
|
325 | (1) |
|
|
325 | (1) |
|
16.62 Plasma engine types |
|
|
325 | (1) |
|
16.63 Plasma propulsion engine |
|
|
326 | (1) |
|
|
326 | (1) |
|
16.65 Platinum rhodium thermocouple |
|
|
326 | (1) |
|
|
326 | (1) |
|
|
326 | (1) |
|
|
326 | (1) |
|
|
327 | (1) |
|
|
328 | (1) |
|
|
328 | (1) |
|
|
328 | (1) |
|
16.73 Pneumatic actuators |
|
|
329 | (1) |
|
|
329 | (1) |
|
|
329 | (1) |
|
|
329 | (1) |
|
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329 | (1) |
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16.78 Point rectilinear vortex |
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329 | (1) |
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330 | (1) |
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330 | (1) |
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330 | (1) |
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330 | (1) |
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16.83 Potential core region |
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330 | (1) |
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331 | (1) |
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331 | (1) |
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16.86 Potential flow past a two-dimensional circular cylinder |
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331 | (1) |
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332 | (1) |
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16.88 Prandtl--Glauert transformation |
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332 | (1) |
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16.89 Prandtl--Meyer expansion |
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332 | (1) |
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16.90 Prandtl--Meyer function |
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332 | (1) |
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16.91 Prandtl's mixing length theory |
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333 | (1) |
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333 | (1) |
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333 | (1) |
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334 | (1) |
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334 | (1) |
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334 | (1) |
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334 | (1) |
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334 | (1) |
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335 | (1) |
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16.100 Pressure coefficient |
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335 | (1) |
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335 | (1) |
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335 | (1) |
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336 | (1) |
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16.104 Pressure-gradient force |
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336 | (1) |
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336 | (1) |
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336 | (1) |
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16.107 Pressure in LPG cylinder |
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336 | (1) |
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16.108 Pressures in the body |
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336 | (1) |
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16.109 Pressure measurement |
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337 | (1) |
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16.110 Pressure measuring devices |
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337 | (1) |
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16.111 Pressure recovery factor |
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337 | (1) |
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16.112 Pressure-regulating valve |
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337 | (1) |
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16.113 Pressure relief valve |
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338 | (1) |
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16.114 Pressure transducers |
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338 | (1) |
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16.115 Preston/Stanton tubes |
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338 | (1) |
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339 | (1) |
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339 | (1) |
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339 | (1) |
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339 | (1) |
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339 | (1) |
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339 | (1) |
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340 | (1) |
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340 | (1) |
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16.124 Propeller efficiency |
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340 | (1) |
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341 | (1) |
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341 | (1) |
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341 | (1) |
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341 | (1) |
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341 | (1) |
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16.130 Pulsed plasma thruster |
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342 | (1) |
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342 | (1) |
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342 | (1) |
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16.133 Pump-turbine hydraulic machines |
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342 | (1) |
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342 | (1) |
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343 | (1) |
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343 | (1) |
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343 | (1) |
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343 | (1) |
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343 | (1) |
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343 | (1) |
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344 | (1) |
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17 Quality of Energy to Quasi-One-Dimensional Flow |
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345 | (2) |
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345 | (1) |
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17.2 Quantised levels of different modes of energy |
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345 | (1) |
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345 | (1) |
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345 | (1) |
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17.5 Quasi-equilibrium process |
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346 | (1) |
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17.6 Quasi-one-dimensional flow |
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346 | (1) |
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347 | (22) |
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347 | (1) |
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347 | (1) |
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347 | (1) |
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347 | (1) |
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347 | (1) |
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348 | (1) |
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348 | (1) |
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348 | (1) |
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348 | (1) |
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348 | (2) |
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350 | (1) |
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350 | (1) |
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18.13 Range of an aircraft |
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350 | (1) |
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351 | (1) |
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18.15 Rankine's half-body |
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351 | (1) |
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352 | (1) |
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352 | (1) |
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18.18 Ranque--Hilsch vortex tube |
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352 | (1) |
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352 | (1) |
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18.20 Rarefied gas dynamics |
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353 | (1) |
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18.21 Rathakrishnan limit |
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353 | (1) |
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18.22 Ratio of specific heats |
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353 | (1) |
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353 | (1) |
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354 | (1) |
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18.25 Rayleigh supersonic pitot formula |
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354 | (1) |
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354 | (1) |
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354 | (1) |
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355 | (1) |
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355 | (1) |
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18.30 Real-gas equation of state |
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355 | (1) |
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18.31 Reciprocating engine |
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355 | (1) |
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355 | (1) |
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18.33 Rectangular aerofoil |
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355 | (1) |
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356 | (1) |
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18.35 Reduced-gravity aircraft |
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356 | (1) |
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356 | (1) |
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18.37 Reduced temperature |
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356 | (1) |
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18.38 Reflexed camber aerofoil |
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356 | (1) |
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356 | (1) |
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356 | (1) |
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357 | (1) |
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357 | (1) |
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357 | (1) |
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357 | (1) |
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18.45 Regimes of fluid mechanics |
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357 | (1) |
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357 | (1) |
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358 | (1) |
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358 | (1) |
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358 | (1) |
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358 | (1) |
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18.51 Resistance temperature detector |
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|
358 | (1) |
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359 | (1) |
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359 | (1) |
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359 | (1) |
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359 | (1) |
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18.56 Reversible adiabatic process |
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359 | (1) |
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359 | (1) |
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360 | (1) |
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360 | (1) |
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18.60 Reynolds experiment |
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360 | (1) |
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360 | (1) |
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361 | (1) |
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361 | (1) |
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361 | (1) |
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361 | (1) |
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362 | (1) |
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18.67 Right hydraulic jump |
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362 | (1) |
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362 | (1) |
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362 | (1) |
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362 | (1) |
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18.71 Rocket engine nozzle |
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363 | (1) |
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363 | (1) |
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363 | (1) |
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18.74 Rohsenow correlation |
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363 | (1) |
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18.75 Role of large-scale structures in subsonic mixing enhancement |
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364 | (1) |
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18.76 Role of shear layer in flow control |
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364 | (1) |
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364 | (1) |
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364 | (1) |
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364 | (1) |
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365 | (1) |
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365 | (1) |
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366 | (1) |
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366 | (1) |
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366 | (1) |
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18.85 Rotational speed of the Earth |
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367 | (1) |
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18.86 Rotating-vane meter |
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|
367 | (1) |
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367 | (1) |
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|
368 | (1) |
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369 | (58) |
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|
369 | (1) |
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369 | (1) |
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|
369 | (1) |
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369 | (1) |
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370 | (1) |
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370 | (1) |
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370 | (1) |
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|
370 | (1) |
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370 | (1) |
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19.10 Saturation pressure |
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370 | (1) |
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|
371 | (1) |
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19.12 Saturation temperature |
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|
371 | (1) |
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|
371 | (1) |
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|
371 | (1) |
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|
371 | (1) |
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19.16 Schlieren technique |
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|
371 | (1) |
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|
372 | (1) |
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|
372 | (1) |
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|
372 | (1) |
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|
372 | (1) |
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|
372 | (1) |
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19.22 Second law of thermodynamics |
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|
372 | (1) |
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|
373 | (1) |
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|
373 | (1) |
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|
373 | (1) |
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|
373 | (1) |
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|
373 | (1) |
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|
374 | (1) |
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374 | (1) |
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374 | (1) |
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19.31 Semi-infinite vortex |
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|
374 | (1) |
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|
374 | (1) |
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374 | (1) |
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374 | (1) |
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375 | (1) |
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|
375 | (1) |
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375 | (1) |
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|
376 | (1) |
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|
376 | (1) |
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|
376 | (1) |
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|
376 | (1) |
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|
376 | (1) |
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|
376 | (1) |
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|
377 | (1) |
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|
377 | (1) |
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19.46 Shallow water effects |
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|
377 | (1) |
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|
377 | (1) |
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|
377 | (1) |
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377 | (1) |
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|
378 | (1) |
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|
378 | (1) |
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|
378 | (1) |
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|
378 | (1) |
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|
379 | (1) |
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19.55 Shock-associated noise |
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|
379 | (1) |
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|
379 | (1) |
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19.57 Shock detachment distance |
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|
380 | (1) |
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19.58 Shock detachment Mach number |
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|
380 | (1) |
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|
380 | (1) |
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19.60 Shock-expansion theory |
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|
380 | (1) |
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|
381 | (1) |
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|
381 | (1) |
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|
381 | (1) |
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|
381 | (1) |
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|
381 | (1) |
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|
382 | (1) |
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|
382 | (1) |
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|
382 | (1) |
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|
382 | (1) |
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|
382 | (1) |
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|
382 | (1) |
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|
382 | (1) |
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|
383 | (1) |
|
19.74 Simple-compressible substance |
|
|
383 | (1) |
|
19.75 Simple-compressible system |
|
|
384 | (1) |
|
19.76 Simple distillation |
|
|
384 | (1) |
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19.77 Simple harmonic motion |
|
|
384 | (1) |
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|
384 | (1) |
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|
384 | (1) |
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|
384 | (1) |
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|
385 | (1) |
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19.82 Simple and nonsimple regions |
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|
385 | (1) |
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|
385 | (1) |
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|
385 | (1) |
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|
386 | (1) |
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|
386 | (1) |
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|
386 | (1) |
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|
387 | (1) |
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|
387 | (1) |
|
19.90 Slant hydraulic jump |
|
|
387 | (1) |
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|
387 | (1) |
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|
387 | (1) |
|
19.93 Slender-body theory |
|
|
387 | (1) |
|
19.94 Slender wing theory |
|
|
388 | (1) |
|
|
388 | (1) |
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|
388 | (1) |
|
|
389 | (1) |
|
19.98 Slowest flying bird |
|
|
389 | (1) |
|
|
389 | (1) |
|
|
389 | (1) |
|
19.101 Small-density-ratio assumption |
|
|
390 | (1) |
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|
390 | (1) |
|
19.103 Small perturbation theory |
|
|
390 | (1) |
|
|
390 | (1) |
|
|
391 | (1) |
|
19.106 Smoke flow visualisation |
|
|
391 | (1) |
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|
391 | (1) |
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|
391 | (1) |