Effects of stress concentration, deflection, and vibration on life of parts subjected to repeated loading are analyzed; criteria established at Consolidated Vultee Aircraft, based on actual fatigue tests of parts involved compared to life at time of failure in service, are discussed; typical examples given. From paper before Inst Aeronautical Sciences.
Fatigue failure of aircraft parts -- Their cause and cure
Automotive Aviation Industries
Automotive and Aviation Industries ; 92 , n 9
1945
Article (Journal)
English
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