A Method for Determining the “Safe” Life of an Aircraft Wing From Fatigue Test Results

Alison Kennedy · Journal of the Royal Aeronautical Society · 1954

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Type: article
Published: 1954-05-01
Cited by: 6
References: 4
DOI: https://doi.org/10.1017/s0368393100106728
OpenAlex: https://openalex.org/W2477028916
Semantic Scholar: https://api.semanticscholar.org/CorpusID:113899316

Keywords

Boom, Wing, Structural engineering, Wing loading, Tension (geology)

References

INVESTIGATION OF STATISTICAL NATURE OF FATIGUE PROPERTIESE. Epremian, Robert F. Mehl — 1952
Statistical Theory with Engineering ApplicationsAlbert H. Bowker, A. Hald — 1952
Fatigue Life of Wing Components for Civil AircraftKeri Williams — 1952
Statistical Theory with Engineering ApplicationsA. Hald, Bernard Friedman — 1953

Cited by

The effect of fatigue cracks on fastener flexibility, load distribution, and fatigue crack growthZachary Layne Whitman — 2012
A BIBLIOGRAPHY ON LIFE TESTING AND RELATED TOPICSWilliam M. Mendenhall — 1958
Full-scale fatigue test of twin-turboprop transportTadao KAMIYAMA, Kazuyuki Takeuchi, Fumio Shima — 1966
The Second Barnwell Memorial Lecture: The Outlook on Airframe FatigueWalter Tye — 1955
Airworthiness and the Air Registration BoardWalter Tye — 1970
Cumulative damage in fatigueE. C. Wilkins — 1956

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