Preliminary information on the complex subject of the fatigue strength of fabricated structural members for aircraft is presented in the test results obtained on several different types of airship girders subjected to axial tension and compression in a resonance fatigue machine. A description of this machine as well as numerous photographs of the fatigue failures are given. There is also presented an extended bibliography on the subject of fatigue strength.
Preliminary Fatigue Studies on Aluminum Alloy Aircraft Girders
1938-02-01
Miscellaneous
No indication
English
Preliminary fatigue studies on aluminum alloy aircraft girders
Engineering Index Backfile | 1938
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