| Preface |
|
xi | |
| Introduction |
|
xiii | |
|
Chapter 1 Aircraft Design |
|
|
1 | (16) |
|
Military Standard---(Mil-Std-1530C) Aircraft Structural Integrity Program |
|
|
2 | (2) |
|
Military Standard---(Mil-Std-882E) Standard Practice for System Safety |
|
|
4 | (1) |
|
Military Standard---(Mil-Std-8861B) Airplane Strength and Rigidity Flight Loads |
|
|
4 | (2) |
|
Military Standard---(MIL-A-8870C) Airplane Strength and Rigidity, Vibration, Flutter, and Divergence |
|
|
6 | (8) |
|
|
|
14 | (1) |
|
|
|
15 | (2) |
|
Chapter 2 Aircraft Material |
|
|
17 | (12) |
|
|
|
17 | (3) |
|
Materials Used in Aircraft Construction |
|
|
20 | (3) |
|
Nonmetallic Aircraft Materials |
|
|
23 | (2) |
|
Materials of Aircraft Hardware |
|
|
25 | (2) |
|
Materials---Aircraft Lubricants |
|
|
27 | (1) |
|
|
|
27 | (1) |
|
|
|
28 | (1) |
|
Chapter 3 Loads on the Aircraft |
|
|
29 | (22) |
|
|
|
29 | (4) |
|
|
|
33 | (2) |
|
Moment, Moment Arm, and Torque |
|
|
35 | (1) |
|
The Vector and Vector Components |
|
|
36 | (1) |
|
Lift Pressure and Wing Loading |
|
|
37 | (1) |
|
Centripetal and Centrifugal Forces |
|
|
38 | (1) |
|
|
|
39 | (2) |
|
|
|
41 | (2) |
|
Fuel Tank Loads during Emergency Landing |
|
|
43 | (1) |
|
|
|
44 | (2) |
|
|
|
46 | (2) |
|
|
|
48 | (1) |
|
|
|
49 | (2) |
|
Chapter 4 Stress Analysis |
|
|
51 | (16) |
|
Strain and Stress-Strain Relations |
|
|
51 | (3) |
|
|
|
54 | (1) |
|
|
|
55 | (3) |
|
Fatigue-Stress Concentration |
|
|
58 | (2) |
|
Behavior of Materials under Stress |
|
|
60 | (1) |
|
Factors Affecting Elastic Properties |
|
|
61 | (1) |
|
|
|
62 | (1) |
|
Elasticity; Proportionality of Stress and Strain |
|
|
62 | (2) |
|
|
|
64 | (1) |
|
|
|
65 | (1) |
|
|
|
66 | (1) |
|
Chapter 5 Torsion, Compression, and Bending Loads |
|
|
67 | (12) |
|
|
|
67 | (1) |
|
|
|
68 | (1) |
|
|
|
69 | (1) |
|
|
|
70 | (1) |
|
Compressive Strength and Failures |
|
|
71 | (2) |
|
|
|
73 | (1) |
|
Elastic Stability---General Condition |
|
|
74 | (1) |
|
|
|
75 | (2) |
|
Nonuniform Loading of Circular Plates |
|
|
77 | (1) |
|
Flat-Plate Ultimate Strength |
|
|
77 | (1) |
|
|
|
77 | (1) |
|
|
|
78 | (1) |
|
Chapter 6 Aircraft Structure Riveted Joints and Pressure Vessels |
|
|
79 | (14) |
|
|
|
79 | (1) |
|
|
|
80 | (1) |
|
Modes of Failure in Riveted Joints |
|
|
80 | (2) |
|
|
|
82 | (1) |
|
Eccentric Loading of Riveted Joints |
|
|
83 | (1) |
|
Stress Analysis of Riveted Joints |
|
|
83 | (1) |
|
Riveted Joints---Common Terms |
|
|
84 | (1) |
|
Pressure Vessels and Pressure Lines |
|
|
84 | (1) |
|
|
|
85 | (1) |
|
|
|
86 | (3) |
|
Difference between Pneumatic and Hydraulic Systems |
|
|
89 | (2) |
|
|
|
91 | (1) |
|
|
|
91 | (2) |
|
Chapter 7 Heat Treatment of Aircraft Metals |
|
|
93 | (22) |
|
|
|
93 | (1) |
|
|
|
94 | (1) |
|
|
|
95 | (4) |
|
Time, Temperature, and Transformation |
|
|
99 | (1) |
|
Continuous Cooling Transformation |
|
|
100 | (1) |
|
Difference between TTT and CCT |
|
|
101 | (1) |
|
|
|
102 | (1) |
|
Aluminum and Aluminum Alloys |
|
|
102 | (1) |
|
|
|
103 | (2) |
|
Magnesium and Magnesium Alloys |
|
|
105 | (1) |
|
Titanium and Titanium Alloys |
|
|
105 | (2) |
|
|
|
107 | (1) |
|
|
|
108 | (1) |
|
Substitution of Aircraft Metals |
|
|
108 | (1) |
|
Cold-Working and Hardening |
|
|
109 | (1) |
|
|
|
110 | (1) |
|
|
|
111 | (2) |
|
|
|
113 | (1) |
|
|
|
113 | (2) |
|
Chapter 8 Aircraft Fatigue and Aircraft Material Fatigue |
|
|
115 | (12) |
|
|
|
115 | (1) |
|
Fatigue Testing (S-N Curve) |
|
|
116 | (1) |
|
|
|
117 | (1) |
|
Military Standard---(Mil-A-83444) Airplane Damage Tolerance Requirements |
|
|
118 | (2) |
|
Stress-Corrosion Cracking |
|
|
120 | (1) |
|
Control of Stress-Corrosion Cracking |
|
|
121 | (1) |
|
|
|
122 | (2) |
|
|
|
124 | (1) |
|
|
|
125 | (2) |
|
Chapter 9 Aircraft Corrosion |
|
|
127 | (20) |
|
|
|
127 | (1) |
|
|
|
128 | (2) |
|
|
|
130 | (3) |
|
|
|
133 | (1) |
|
|
|
134 | (1) |
|
|
|
134 | (2) |
|
|
|
136 | (1) |
|
Corrosion of Ferrous Metals |
|
|
137 | (1) |
|
Factors Affecting Corrosion |
|
|
138 | (1) |
|
Corrosion-Prone Areas in Aircraft |
|
|
139 | (2) |
|
Factors in Corrosion Control |
|
|
141 | (1) |
|
Corrosion Inspection and Detection |
|
|
142 | (1) |
|
Preventive Maintenance of Corrosion |
|
|
143 | (1) |
|
|
|
144 | (1) |
|
|
|
145 | (2) |
|
Chapter 10 Dynamic Stress, Temperature Stress, and Experimental Methods |
|
|
147 | (8) |
|
|
|
147 | (2) |
|
Remarks on Stress due to Impact |
|
|
149 | (1) |
|
|
|
149 | (1) |
|
|
|
150 | (2) |
|
Stress Pattern Analysis by Thermal Emission |
|
|
152 | (1) |
|
|
|
153 | (1) |
|
|
|
153 | (2) |
|
|
|
155 | (18) |
|
Applications of Composites on Aircraft |
|
|
155 | (1) |
|
Fiber-Reinforced Materials |
|
|
156 | (2) |
|
Laminar or Laminated Composites |
|
|
158 | (1) |
|
Particulate-Reinforced Composites |
|
|
159 | (1) |
|
Mechanics of Composite Material |
|
|
160 | (1) |
|
Stress and Strain in a Laminate |
|
|
160 | (1) |
|
Composite Fatigue and Damage Tolerance |
|
|
161 | (1) |
|
Aircraft Accident--Crashworthiness |
|
|
162 | (3) |
|
|
|
165 | (1) |
|
Composite Manufacturing and In-Service Defects and Damages |
|
|
165 | (3) |
|
Composite Maintenance and Inspection |
|
|
168 | (1) |
|
|
|
169 | (1) |
|
|
|
169 | (1) |
|
|
|
170 | (3) |
|
Chapter 12 Nondestructive Testing and Nondestructive Inspection |
|
|
173 | (26) |
|
|
|
175 | (1) |
|
|
|
175 | (2) |
|
Liquid Penetrant (Dye Penetrant) Inspection |
|
|
177 | (2) |
|
Magnetic Particle Inspection |
|
|
179 | (5) |
|
Radiographic Inspection (X-Rays and Gamma Rays) |
|
|
184 | (4) |
|
|
|
188 | (3) |
|
|
|
191 | (6) |
|
|
|
197 | (1) |
|
|
|
198 | (1) |
|
Chapter 13 Aviation Maintenance Management |
|
|
199 | (22) |
|
|
|
199 | (6) |
|
Typical Airline Definition of Maintenance |
|
|
205 | (1) |
|
Goals of a Maintenance Program |
|
|
205 | (1) |
|
Functional and Potential Failure |
|
|
205 | (1) |
|
Documentation for Maintenance |
|
|
206 | (2) |
|
Requirements for a Maintenance Program |
|
|
208 | (3) |
|
Material Support---Stores and Logistics |
|
|
211 | (2) |
|
Material Department---Budgeting Efforts |
|
|
213 | (1) |
|
|
|
214 | (1) |
|
|
|
214 | (1) |
|
|
|
215 | (1) |
|
|
|
215 | (3) |
|
|
|
218 | (1) |
|
|
|
219 | (1) |
|
|
|
219 | (2) |
|
Chapter 14 Case Studies and Human Factors |
|
|
221 | (32) |
|
Case Study 14-1 TWA Flight 843 |
|
|
221 | (5) |
|
Case Study 14-2 Atlantic Southeast Airlines Flight 2311 |
|
|
226 | (6) |
|
Case Study 14-3 United Airlines Flight 232 |
|
|
232 | (9) |
|
Case Study 14-4 American Airlines Flight 191 |
|
|
241 | (5) |
|
Case Study 14-5 USAir Flight 427 |
|
|
246 | (2) |
|
|
|
248 | (1) |
|
Human Factors in Aircraft Maintenance |
|
|
248 | (2) |
|
Maintenance Error Decision Aid |
|
|
250 | (1) |
|
|
|
251 | (1) |
|
|
|
252 | (1) |
Answers to
Chapter Questions |
|
253 | (8) |
| Index |
|
261 | |
Lisainfo e-raamatute kohta