Use of periodic microstructure observations as possible supplement to existing inspection techniques for aircraft wheels and as indicator of expended fatigue life; dye penetrant, eddy current, and replica (or microscopic) inspection techniques were performed at 10% increments of estimated fatigue life; results showed that microstructure did not change significantly during dynamometer testing and that eddy current and replica techniques were more sensitive; no practical assessment of expended fatigue life can be gained by monitoring microstructure.
Dynamometer evaluation of aircraft wheel microinspection techniques
SAE -- Paper
SAE Meeting ; 1962
1962
7 pages
Aufsatz (Konferenz)
Englisch
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