Paper presents fatigue problem that developed in empennage area of Navy A3D aircraft, ground and flight test programs undertaken, and results; five areas where acoustical fatigue occurred most frequently and type and size of material listed; effective solution to cracking problem found was addition of elastomer at point where cracks occurred; procedure whereby tests results may be incorporated with analytical analysis to produce curves for design analysis. (See also SAE -- Paper for meeting n 164A Apr 5-8 1960 23 p)
Acoustically induced fatigue -- Cause, solution and design analysis
SAE -- J
Society of Automotive Engineers -- Journal ; 68 , n 7
1960
4 pages
Aufsatz (Zeitschrift)
Englisch
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