| Preface to the Seventh Edition of Aircraft Structures |
|
xv | |
| Part A Fundamentals Of Structural Analysis |
|
|
|
|
3 | (94) |
|
Chapter 1 Basic elasticity |
|
|
5 | (48) |
|
|
|
5 | (2) |
|
1.2 Notation for forces and stresses |
|
|
7 | (2) |
|
1.3 Equations of equilibrium |
|
|
9 | (2) |
|
|
|
11 | (1) |
|
|
|
11 | (1) |
|
1.6 Determination of stresses on inclined planes |
|
|
12 | (4) |
|
|
|
16 | (2) |
|
1.8 Mohr's circle of stress |
|
|
18 | (6) |
|
|
|
24 | (4) |
|
1.10 Compatibility equations |
|
|
28 | (1) |
|
|
|
29 | (1) |
|
1.12 Determination of strains on inclined planes |
|
|
29 | (3) |
|
|
|
32 | (1) |
|
1.14 Mohr's circle of strain |
|
|
32 | (1) |
|
1.15 Stress-strain relationships |
|
|
32 | (10) |
|
1.16 Experimental measurement of surface strains |
|
|
42 | (6) |
|
|
|
48 | (1) |
|
|
|
48 | (1) |
|
|
|
48 | (5) |
|
Chapter 2 Two-dimensional problems in elasticity |
|
|
53 | (22) |
|
2.1 Two-dimensional problems |
|
|
53 | (2) |
|
|
|
55 | (1) |
|
2.3 Inverse and semi-inverse methods |
|
|
56 | (7) |
|
2.4 St. Venant's principle |
|
|
63 | (1) |
|
|
|
64 | (1) |
|
2.6 Bending of an end-loaded cantilever |
|
|
64 | (6) |
|
|
|
70 | (1) |
|
|
|
70 | (5) |
|
Chapter 3 Torsion of solid sections |
|
|
75 | (22) |
|
3.1 Prandtl stress function solution |
|
|
75 | (13) |
|
3.2 St. Venant warping function solution |
|
|
88 | (1) |
|
|
|
89 | (2) |
|
3.4 Torsion of a narrow rectangular strip |
|
|
91 | (3) |
|
|
|
94 | (1) |
|
|
|
94 | (3) |
|
Section A2 Virtual work, energy, and matrix methods |
|
|
97 | (146) |
|
Chapter 4 Virtual work and energy methods |
|
|
99 | (32) |
|
|
|
99 | (1) |
|
4.2 Principle of virtual work |
|
|
100 | (14) |
|
4.3 Applications of the principle of virtual work |
|
|
114 | (11) |
|
|
|
125 | (1) |
|
|
|
126 | (5) |
|
|
|
131 | (62) |
|
5.1 Strain energy and complementary energy |
|
|
131 | (2) |
|
5.2 Principle of the stationary value of the total complementary energy |
|
|
133 | (1) |
|
5.3 Application to deflection problems |
|
|
134 | (10) |
|
5.4 Application to the solution of statically indeterminate systems |
|
|
144 | (18) |
|
|
|
162 | (2) |
|
|
|
164 | (5) |
|
5.7 Total potential energy |
|
|
169 | (1) |
|
5.8 Principle of the stationary value of the total potential energy |
|
|
170 | (4) |
|
5.9 Principle of superposition |
|
|
174 | (1) |
|
|
|
174 | (4) |
|
|
|
178 | (2) |
|
|
|
180 | (1) |
|
|
|
180 | (1) |
|
|
|
181 | (12) |
|
|
|
193 | (50) |
|
|
|
194 | (1) |
|
6.2 Stiffness matrix for an elastic spring |
|
|
195 | (1) |
|
6.3 Stiffness matrix for two elastic springs in line |
|
|
196 | (3) |
|
6.4 Matrix analysis of pin-jointed frameworks |
|
|
199 | (8) |
|
6.5 Application to statically indeterminate frameworks |
|
|
207 | (1) |
|
6.6 Matrix analysis of space frames |
|
|
207 | (2) |
|
6.7 Stiffness matrix for a uniform beam |
|
|
209 | (7) |
|
6.8 Finite element method for continuum structures |
|
|
216 | (17) |
|
|
|
233 | (1) |
|
|
|
234 | (1) |
|
|
|
234 | (9) |
|
Section A3 Thin plate theory |
|
|
243 | (38) |
|
Chapter 7 Bending of thin plates |
|
|
245 | (36) |
|
7.1 Pure bending of thin plates |
|
|
245 | (3) |
|
7.2 Plates subjected to bending and twisting |
|
|
248 | (4) |
|
7.3 Plates subjected to a distributed transverse load |
|
|
252 | (11) |
|
7.4 Combined bending and in-plane loading of a thin rectangular plate |
|
|
263 | (4) |
|
7.5 Bending of thin plates having a small initial curvature |
|
|
267 | (1) |
|
7.6 Energy method for the bending of thin plates |
|
|
267 | (9) |
|
|
|
276 | (1) |
|
|
|
276 | (5) |
|
Section A4 Structural instability |
|
|
281 | (88) |
|
|
|
283 | (48) |
|
8.1 Euler buckling of columns |
|
|
283 | (8) |
|
|
|
291 | (5) |
|
8.3 Effect of initial imperfections |
|
|
296 | (4) |
|
8.4 Stability of beams under transverse and axial loads |
|
|
300 | (4) |
|
8.5 Energy method for the calculation of buckling loads in columns |
|
|
304 | (4) |
|
8.6 Flexural-torsional buckling of thin-walled columns |
|
|
308 | (12) |
|
|
|
320 | (1) |
|
|
|
320 | (11) |
|
|
|
331 | (38) |
|
9.1 Buckling of thin plates |
|
|
331 | (4) |
|
9.2 Inelastic buckling of plates |
|
|
335 | (2) |
|
9.3 Experimental determination of the critical load for a flat plate |
|
|
337 | (1) |
|
|
|
337 | (1) |
|
9.5 Instability of stiffened panels |
|
|
338 | (2) |
|
9.6 Failure stress in plates and stiffened panels |
|
|
340 | (7) |
|
|
|
347 | (15) |
|
|
|
362 | (1) |
|
|
|
363 | (6) |
|
Section A5 Vibration of structures |
|
|
369 | (26) |
|
Chapter 10 Structural vibration |
|
|
371 | (24) |
|
10.1 Oscillation of mass-spring systems |
|
|
371 | (10) |
|
10.2 Oscillation of beams |
|
|
381 | (5) |
|
10.3 Approximate methods for determining natural frequencies |
|
|
386 | (3) |
|
|
|
389 | (6) |
| Part B Analysis Of Aircraft Structures |
|
|
Section B1 Principles of stressed skin construction |
|
|
395 | (52) |
|
|
|
397 | (24) |
|
|
|
397 | (2) |
|
|
|
399 | (1) |
|
|
|
400 | (1) |
|
|
|
401 | (1) |
|
|
|
401 | (1) |
|
|
|
401 | (1) |
|
|
|
402 | (1) |
|
11.8 Properties of materials |
|
|
403 | (15) |
|
|
|
418 | (3) |
|
Chapter 12 Structural components of aircraft and spacecraft |
|
|
421 | (26) |
|
12.1 Structural components: Aircraft |
|
|
421 | (12) |
|
12.2 Structural components: Spacecraft |
|
|
433 | (3) |
|
|
|
436 | (7) |
|
|
|
443 | (1) |
|
|
|
444 | (3) |
|
Section B2 Airworthiness and airframe loads |
|
|
447 | (62) |
|
|
|
449 | (6) |
|
13.1 Factors of safety: Flight envelope |
|
|
449 | (2) |
|
13.2 Load factor determination |
|
|
451 | (2) |
|
13.3 Airworthiness: Spacecraft |
|
|
453 | (1) |
|
|
|
454 | (1) |
|
|
|
454 | (1) |
|
Chapter 14 Airframe loads |
|
|
455 | (30) |
|
14.1 Aircraft inertia loads |
|
|
455 | (6) |
|
14.2 Symmetric maneuver loads |
|
|
461 | (5) |
|
14.3 Normal accelerations associated with various types of maneuver |
|
|
466 | (4) |
|
|
|
470 | (8) |
|
14.5 Design loads: Spacecraft |
|
|
478 | (1) |
|
|
|
478 | (1) |
|
|
|
479 | (6) |
|
|
|
485 | (24) |
|
15.1 Safe life and fail-safe structures |
|
|
485 | (1) |
|
15.2 Designing against fatigue |
|
|
486 | (1) |
|
15.3 Fatigue strength of components |
|
|
487 | (6) |
|
15.4 Prediction of aircraft fatigue life |
|
|
493 | (6) |
|
|
|
499 | (7) |
|
|
|
506 | (1) |
|
|
|
506 | (1) |
|
|
|
507 | (2) |
|
Section B3 Bending, shear, and torsion of thin-walled beams |
|
|
509 | (160) |
|
Chapter 16 Bending of open and closed thin-walled beams |
|
|
511 | (62) |
|
|
|
512 | (9) |
|
16.2 Unsymmetrical bending |
|
|
521 | (8) |
|
16.3 Deflections due to bending |
|
|
529 | (20) |
|
16.4 Calculation of section properties |
|
|
549 | (10) |
|
16.5 Applicability of bending theory |
|
|
559 | (1) |
|
|
|
559 | (4) |
|
|
|
563 | (1) |
|
|
|
563 | (10) |
|
Chapter 17 Shear of beams |
|
|
573 | (32) |
|
17.1 General stress, strain, and displacement relationships for open and single-cell closed section thin-walled beams |
|
|
573 | (4) |
|
17.2 Shear of open section beams |
|
|
577 | (9) |
|
17.3 Shear of closed section beams |
|
|
586 | (9) |
|
|
|
595 | (1) |
|
|
|
595 | (10) |
|
Chapter 18 Torsion of beams |
|
|
605 | (24) |
|
18.1 Torsion of closed section beams |
|
|
605 | (10) |
|
18.2 Torsion of open section beams |
|
|
615 | (6) |
|
|
|
621 | (8) |
|
Chapter 19 Combined open and closed section beams |
|
|
629 | (12) |
|
|
|
629 | (2) |
|
|
|
631 | (3) |
|
|
|
634 | (5) |
|
|
|
639 | (2) |
|
Chapter 20 Structural idealization |
|
|
641 | (28) |
|
|
|
641 | (1) |
|
20.2 Idealization of a panel |
|
|
642 | (4) |
|
20.3 Effect of idealization on the analysis of open and closed section beams |
|
|
646 | (13) |
|
20.4 Deflection of open and closed section beams |
|
|
659 | (3) |
|
|
|
662 | (7) |
|
Section B4 Stress analysis of aircraft and spacecraft components |
|
|
669 | (146) |
|
Chapter 21 Wing spars and box beams |
|
|
671 | (18) |
|
|
|
671 | (4) |
|
21.2 Open and closed section beams |
|
|
675 | (5) |
|
21.3 Beams having variable stringer areas |
|
|
680 | (5) |
|
|
|
685 | (4) |
|
|
|
689 | (22) |
|
|
|
689 | (2) |
|
|
|
691 | (2) |
|
|
|
693 | (2) |
|
22.4 Pressurized fuselages |
|
|
695 | (7) |
|
22.5 Cut-outs in fuselages |
|
|
702 | (5) |
|
|
|
707 | (1) |
|
|
|
707 | (4) |
|
|
|
711 | (34) |
|
|
|
711 | (1) |
|
|
|
712 | (2) |
|
|
|
714 | (4) |
|
|
|
718 | (7) |
|
|
|
725 | (1) |
|
|
|
725 | (3) |
|
|
|
728 | (1) |
|
|
|
729 | (8) |
|
|
|
737 | (8) |
|
Chapter 24 Fuselage frames and wing ribs |
|
|
745 | (12) |
|
24.1 Principles of stiffener/web construction |
|
|
745 | (5) |
|
|
|
750 | (1) |
|
|
|
751 | (4) |
|
|
|
755 | (2) |
|
|
|
757 | (6) |
|
|
|
757 | (1) |
|
|
|
758 | (1) |
|
|
|
759 | (2) |
|
|
|
761 | (1) |
|
|
|
761 | (2) |
|
Chapter 26 Laminated composite structures |
|
|
763 | (52) |
|
26.1 Elastic constants of a simple lamina |
|
|
763 | (6) |
|
26.2 Stress-strain relationships for an orthotropic ply (macro approach) |
|
|
769 | (9) |
|
|
|
778 | (17) |
|
26.4 Thin-walled composite beams |
|
|
795 | (13) |
|
|
|
808 | (1) |
|
|
|
808 | (7) |
|
Section B5 Structural and loading discontinuities |
|
|
815 | (70) |
|
Chapter 27 Closed section beams |
|
|
817 | (42) |
|
|
|
817 | (1) |
|
27.2 Shear stress distribution at a built-in end of a closed section beam |
|
|
818 | (6) |
|
27.3 Thin-walled rectangular section beam subjected to torsion |
|
|
824 | (8) |
|
|
|
832 | (17) |
|
|
|
849 | (1) |
|
|
|
849 | (10) |
|
Chapter 28 Open section beams |
|
|
859 | (26) |
|
28.1 I-Section beam subjected to torsion |
|
|
859 | (2) |
|
28.2 Torsion of an arbitrary section beam |
|
|
861 | (10) |
|
28.3 Distributed torque loading |
|
|
871 | (2) |
|
28.4 Extension of the theory to allow for general systems of loading |
|
|
873 | (3) |
|
28.5 Moment couple (bimoment) |
|
|
876 | (3) |
|
|
|
879 | (1) |
|
|
|
879 | (6) |
|
Section B6 Introduction to aeroelasticity |
|
|
885 | (26) |
|
|
|
887 | (24) |
|
|
|
887 | (1) |
|
29.2 Load distribution and divergence |
|
|
888 | (6) |
|
29.3 Control effectiveness and reversal |
|
|
894 | (6) |
|
29.4 Introduction to "flutter" |
|
|
900 | (7) |
|
|
|
907 | (1) |
|
|
|
907 | (4) |
| Appendix: Design of a rear fuselage |
|
911 | (28) |
| Index |
|
939 | |
Biežāk uzdotie jautājumi par e-grāmatām