Այս գրքի մասին
Իմ գրադարանը
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Symmetrical flight conditions (flaps or auxiliary devices in operation) __
5
10
CONTENTS—Continued
Rudder systems_
Aileron systems___
Flap and auxiliary control systems.
Towing and launching (release mechanism) control systems.
Ground loads..
Level landing--
Level landing with side load..
Nose-down landing--
Head-on landing-
Wing-tip landing--
Launching and towing loads__
Loads on fittings- - -
Wing truss strength_
Multiplying factors of safety-
Fittings...
Castings
Parallel double wires__
Wires at small angles.
Double drag trusses..
Torque tubes used as hinges.
Control surface hinges and control system joints.
Wire sizes___
Wing lift trusses_
Page
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35
36
37
38
39
40
41
43
44
Special procedure in limit load tests_
Special procedure in ultimate load tests-
Special procedures when ultimate load tests are conducted in lieu of
stress analysis _ _ _
Check of test structure_
Test report---.
Wing tests
Rib tests--
Selection of ribs__
54
55
57
Wing of uniform chord
Tapered wing--
Test loadings___
Test methods...
Wing proof and strength tests_
Test loads_-.
Test methods_
General__
Mounting-
Chord component__
Deflections_
Rigidity..
Test report--.
Control surface tests_
Tail surface and aileron tests_
Test loads. _ .
Kinds of tests.
Load distribution-tail surfaces-
Ailerons - -
Balance area.
Test methods.
Horns..
Mounting---.
Fabric covering-
Brace wires..
Load application.
Flap tests--
Test methods and loads..
Test report---
Control system tests.
Test loads
Operating test__
Strength tests_
Method of load application--
Application.
Operation test_ _
Ultimate load test_.
Rigidity
Test report--
Fuselage tests.
Test loads..
60
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62
67
71
72
74
75