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E-grāmata: Essentials of Supersonic Commercial Aircraft Conceptual Design [Wiley Online]

(Delft University of Technology), Series edited by (BAE Systems, UK), Series edited by (MIT), Series edited by (University Of Liverpool)
  • Formāts: 184 pages
  • Sērija : Aerospace Series
  • Izdošanas datums: 11-Jun-2020
  • Izdevniecība: John Wiley & Sons Inc
  • ISBN-10: 1119667062
  • ISBN-13: 9781119667063
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  • Wiley Online
  • Cena: 128,28 €*
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Essentials of Supersonic Commercial Aircraft Conceptual DesignPalielināt
  • Formāts: 184 pages
  • Sērija : Aerospace Series
  • Izdošanas datums: 11-Jun-2020
  • Izdevniecība: John Wiley & Sons Inc
  • ISBN-10: 1119667062
  • ISBN-13: 9781119667063
Citas grāmatas par šo tēmu:
Wiley Online E-booksMore info about Wiley Online
Rokasgrāmatas mājas lapa: https://onlinelibrary.wiley.com/doi/book/10.1002/9781119667063

Provides comprehensive coverage of how supersonic commercial aircraft are designed

This must-have guide to conceptual supersonic aircraft design provides a state-of-the art overview of the subject, along with expert analysis and discussion. It examines the challenges of high-speed flight, covers aerodynamic phenomena in supersonic flow and aerodynamic drag in cruising flight, and discusses the advantages and disadvantages of oblique wing aircraft.

Essentials of Supersonic Commercial Aircraft Conceptual Design is intended for members of a team producing an initial design concept of an airliner with the capability of making supersonic cruising flights. It begins with a synopsis of the history of supersonic transport aircraft development and continues with a chapter on the challenges of high-speed flight, which discusses everything from top level requirements and cruise speed requirements to fuel efficiency and cruise altitude. It then covers weight sensitivity; aerodynamic phenomena in supersonic flow; thin wings in two-dimensional flow; flat wings in inviscid supersonic flow; aerodynamic drag in cruising flight, and aerodynamic efficiency of SCV configurations. The book finishes with a chapter that examines oblique wing aircraft.

  • Provides supersonic aircraft designers with everything they need to know about developing current and future high speed commercial jet planes
  • Examines the many challenges of high-speed flight
  • Covers aerodynamic phenomena in supersonic flow and aerodynamic drag in cruising flight
  • Discusses the advantages and disadvantages of oblique wing aircraft 

Essentials of Supersonic Commercial Aircraft Conceptual Design is an ideal book for researchers and practitioners in the aerospace industry, as well as for graduate students in aerospace engineering.

Foreword xi
Series Preface xv
Preface xvii
Acknowledgements xix
1 History Of Supersonic Transport Aircraft Development
1(16)
1.1 Concorde's Development and Service
2(2)
1.2 SST Development Program
4(3)
1.3 Transonic Transport Configuration Studies
7(1)
1.4 US High Speed Research and Development Programs
8(1)
1.5 European Supersonic Research Program
9(2)
1.6 A Market for a Supersonic Commercial Aircraft?
11(6)
1.6.1 Why Fly Supersonically?
11(1)
1.6.2 Requirements and Operations
12(1)
1.6.3 Block Speed, Productivity, and Complexity
13(2)
Bibliography
15(2)
2 The Challenges Of High-Speed Flight
17(12)
2.1 Top Level Requirements (TLR)
18(1)
2.2 The Need for Speed
19(1)
2.3 Cruise Speed Selection
20(3)
2.4 Aerodynamic Design Considerations
23(6)
2.4.1 Fuel and Flight Efficiency
23(1)
2.4.2 Aerodynamic Efficiency
24(1)
2.4.3 Power Plant Efficiency
25(1)
2.4.4 Flight Efficiency
26(1)
2.4.5 Cruise Altitude
27(1)
Bibliography
28(1)
3 Weight Prediction, Optimization, And Energy Efficiency
29(16)
3.1 The Unity Equation
29(1)
3.2 Early Weight Prediction
30(2)
3.2.1 Empty Weight
30(2)
3.3 Fuel Weight
32(2)
3.3.1 Mission Fuel
33(1)
3.3.2 Reserve Fuel
34(1)
3.4 Take-off Weight and the Weight Growth Factor
34(1)
3.5 Example of an Early Weight Prediction
35(3)
3.5.1 MTOW Sensitivity
36(2)
3.6 Productivity and Energy Efficiency
38(7)
3.6.1 Range for Maximum Productivity
39(1)
3.6.2 Energy Efficiency
40(1)
3.6.3 Conclusion
41(1)
Bibliography
42(3)
4 Aerodynamic Phenomena In Supersonic Flow
45(20)
4.1 Compressibility of Atmospheric Air
45(2)
4.1.1 Speed of Sound and Mach Number
46(1)
4.1.2 Compressible and Incompressible Flows
47(1)
4.2 Streamlines and Mach Waves
47(3)
4.2.1 Sound Waves
48(2)
4.3 Shock Waves
50(1)
4.4 Normal Shock Waves
51(2)
4.4.1 Effects of Normal Shock Waves
52(1)
4.5 Planar Oblique Shock Waves
53(3)
4.6 Curved and Detached Shock waves
56(1)
4.7 Expansion Flows
57(2)
4.8 Shock-expansion Technique
59(1)
4.9 Leading-edge Delta Vortices
60(1)
4.10 Sonic Boom
61(4)
Bibliography
62(3)
5 Thin Wings In Two-Dimensional Flow
65(10)
5.1 Small Perturbation Flow
65(10)
5.1.1 Linearized Velocity Potential Equation
66(1)
5.1.2 Pressure Coefficient
67(1)
5.1.3 Lift Gradient
68(1)
5.1.4 Pressure Drag
69(1)
5.1.5 Symmetric Airfoils with Minimum Pressure Drag
70(1)
5.1.6 Total Drag
71(1)
5.1.7 Center of Pressure
72(1)
5.1.8 Concluding Remarks
72(1)
Bibliography
73(2)
6 Flat Wings In Inviscid Supersonic Flow
75(16)
6.1 Classification of Edge Flows
76(1)
6.2 Linear Theory for Three-dimensional Inviscid Flow
76(4)
6.2.1 Flow Reversal Theorems
77(1)
6.2.2 Constant-chord Straight Wings
77(2)
6.2.3 Constant-chord Swept Wings
79(1)
6.3 Slender Wings
80(1)
6.4 Delta Wing
81(5)
6.4.1 Supersonic Leading Edge
82(1)
6.4.2 Subsonic Leading Edge
83(3)
6.5 Arrow Wings
86(1)
6.6 Slender Delta and Arrow Wing Varieties
87(4)
Bibliography
88(3)
7 Aerodynamic Drag In Cruising Flight
91(24)
7.1 Categories of Drag Contributions
91(3)
7.1.1 Miscellaneous Drag Terms and the Concept Drag Area
93(1)
7.1.2 Analysis Methods
93(1)
7.2 Skin Friction Drag
94(3)
7.2.1 Friction Coefficient
95(1)
7.2.2 Flat-plate Analogy
96(1)
7.2.3 Form Drag
97(1)
7.3 Slender Body Wave Drag
97(4)
7.3.1 Conical Forebody Pressure Drag
97(1)
7.3.2 Von Karman's Ogive
98(1)
7.3.3 Sear-Haack Body
99(2)
7.4 Zero-lift Drag of Flat Delta Wings
101(4)
7.4.1 Drag due to Lift
102(1)
7.4.2 Vortex-induced Drag
103(1)
7.4.3 Wave Drag Due to Lift
104(1)
7.5 Wing-alone Glide Ratio
105(4)
7.5.1 Notched Trailing Edges
105(1)
7.5.2 Zero-lift Drag
106(1)
7.5.3 Induced Drag
106(1)
7.5.4 Minimum Glide Ratio
107(2)
7.6 Fuselage-alone Drag
109(6)
7.6.1 Pressure Drag
109(1)
7.6.2 Skin Friction Drag
110(1)
7.6.3 Fuselage Slenderness Ratio
111(1)
Bibliography
112(3)
8 Aerodynamic Efficiency Of Scv Configurations
115(18)
8.1 Interaction Between Configuration Shape and Drag
115(2)
8.2 Configuration (A)
117(4)
8.2.1 Slenderness ratio and lift coefficient for minimum drag
119(1)
8.2.2 Cruise Altitude for Minimum Drag
120(1)
8.3 Configuration B
121(3)
8.3.1 Glide Ratio
122(1)
8.3.2 Cruise Altitude and Wing Loading
123(1)
8.4 Full-configuration Drag
124(3)
8.4.1 Configuration Glide Ratio
125(1)
8.4.2 Notch Ratio Selection
126(1)
8.5 Selection of the General Arrangement
127(6)
8.5.1 Fore-plane Versus After-tail
127(1)
8.5.2 Application of the Area Rule
128(2)
Bibliography
130(3)
9 Aerodynamics Of Cambered Wings
133(10)
9.1 Flat Delta Wing Lift Gradient and Induced Drag
134(4)
9.1.1 Achievable Leading-edge Thrust
138(1)
9.2 Warped Wings
138(5)
Bibliography
140(3)
10 Oblique Wing Aircraft
143(12)
10.1 Advantages of the Oblique Wing
144(1)
10.2 Practical Advantages of the Oblique Wing
145(1)
10.3 Oblique Wing Transport Aircraft
146(1)
10.4 Oblique Flying Wing (OFW)
147(2)
10.4.1 OFW Flying Qualities and Disadvantages
148(1)
10.5 Conventional and OWB Configurations Compared
149(3)
10.5.1 Practical Side-effects
150(2)
10.6 Conclusion
152(3)
Bibliography
153(2)
Index 155
Egbert Torenbeek, PhD, is Professor Emeritus of Aircraft Design at Delft University of Technology. He graduated as an engineer in 1961 at TU Delft and in 1964 he became responsible for teaching the Aircraft Preliminary Design course at the department of Aerospace Engineering. After a sabbatical at Lockheed Georgia Company, he became a senior lecturer and full professor of the Aircraft Design chair at TU Delft, initiating research and teaching in computer-assisted aircraft design.
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