Cumulative damage in fatigue

E. C. Wilkins · 1956

Summary

The aircraft designer today is faced with the necessity of estimating not only the strength of a structure, but also its life — a task with which he was not confronted before.

Published: 1956-01-01
Cited by: 4,883
References: 8
DOI: https://doi.org/10.1007/978-3-642-99854-6_35
Semantic Scholar: https://api.semanticscholar.org/CorpusID:61255831

References

The Failure of Metals by FatigueGeorge Bailey — 1949
Strength of Aeroplanes in Relation to Repeated LoadsD. Williams — 1950
A Method for Determining the “Safe” Life of an Aircraft Wing From Fatigue Test ResultsAlison Kennedy — 1954
Design Criterion for Fatigue of WingsP. B. Walker — 1953
The Estimation of Fatigue Damage in Aircraft Wing StructuresA.H. CHILVER — 1954
The Behaviour of Structures Under Repeated LoadsAlfred Pugsley — 1947
A Photoelastic-Fatigue Programme of Experimental Research in Connection with Bolted JointsEithne Wilkins, H. T. Jessop — 1954
Fatigue Life of Wing Components for Civil AircraftKeri Williams — 1952

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