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 abstract in SAE -- J v 68 n 7 July 1960 p 52-5)
Acoustically induced fatigue -- Cause, solution and design analysis
SAE -- Paper
SAE Meeting ; 1960 Fatigue
1960
23 pages
Aufsatz (Konferenz)
Englisch
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