Results 181 to 190 of about 40,632 (210)
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1984
Damage tolerant design criteria and the current use of random or flight-by-flight loading methods in the full-scale testing of aircraft structures have necessitated the development of new techniques for acquiring accurate fatigue crack growth information from fracture surface analysis.
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Damage tolerant design criteria and the current use of random or flight-by-flight loading methods in the full-scale testing of aircraft structures have necessitated the development of new techniques for acquiring accurate fatigue crack growth information from fracture surface analysis.
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MONITORING OF MULTICOMPONENT CYCLIC LOADING DURING FULL-SCALE FATIGUE TESTS OF AIRCRAFT STRUCTURE
TsAGI Science Journal, 2020Konstantin Stepanovich Shcherban +3 more
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2000
Fourth Symposium on Applications of Automation in Fatigue and and Fracture Testing and Analysis, Orlando ...
Hewitt, R. L., Nelson, A.
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Fourth Symposium on Applications of Automation in Fatigue and and Fracture Testing and Analysis, Orlando ...
Hewitt, R. L., Nelson, A.
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<title>Crack detection on a full-scale aircraft fatigue test</title>
SPIE Proceedings, 1997Ian R. Searle +2 more
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Full-scale fatigue test of unit-plate ballastless track laid on long-span cable-stayed bridge
Construction and Building Materials, 2020Zhi-hui Zhu
exaly
FATIGUE AND RESIDUAL STRENGTH TESTS OF THE FULL-SCALE COMPOSITE WING BOX OF A PASSENGER AIRCRAFT
TsAGI Science Journal, 2019Anna Yurievna Zacharenkova +6 more
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