Effect of some aircraft loading program modifications on the fatigue life of open hole specimens-Reference-Cited by-同舟云学术

Effect of some aircraft loading program modifications on the fatigue life of open hole specimens

Published:1980-01 Issue:2 Volume:13 Page:237-256
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

Buch Alfred

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference25 articles.

1. Flight simulation tests on notched elements;Schijve;NLR TR 74033-U,1974

2. A standardized load sequence for flight simulation tests on transport aircraft wing structures;De Jonge;NLR TR 73029-U—LBF Ber. FB-106,1973

3. Zur Verwendung von Bemessungsunterlagen aus Versuchen mit betriebsähnlichen Lastfolgen zur Lebensdauerabschätzung;Schütz;LBF Bericht Nr FB-109,1976

4. Use of standardized sequences of flight-by-flight load spectra in fatigue testing of structural aircraft Components;Barrois;Engng Fracture Mech.,1977

5. The accumulation of fatigue damage in aircraft materials and structures;Schijve;AGARD-AG-157,1972

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