Report deals with quantitative analyses of fracture surfaces resulting from fatigue failures that occurred in wing structure and lift struts during wing fatigue tests on single engined light aircraft; information concerning rates of propagation and sequence of failure was derived for main spar of wing, subjected to relatively severe load spectrum commensurate with agricultural operations; description of analytical techniques, and results concerning fatigue crack propagation history of main spar structure.
Quantitative fatigue crack propagation analysis by means of electron fractography
Canada. Nat Research Council -- Aeronautical Report
1966
33 pages
Report
Englisch
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