FATIGUE TEST RESULTS AND ANALYSIS OF FOUR PISTON PROVOST WINGS TESTED IN AN ASCENDING-DESCENDING ORDER OF LOADING

Results of fatigue tests on four wings programme loaded in Lo-Hi-Lo order are compared with similar tests performed in Hi-Lo and Lo-Hi orders reported previously. The results lie almost mid-way between the results for Hi-Lo and Lo-Hi tests. No significant difference is shown in either the variance o...

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Bibliographische Detailangaben

1. Verfasser:	Parish,H E
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft CORRELATION TECHNIQUES FAILURE(MECHANICS) FATIGUE(MECHANICS) LIFE EXPECTANCY(SERVICE LIFE) LOADS(FORCES) Mechanics UNITED KINGDOM WINGS
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