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Volume 34, Issue 11
1 November 1962
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 34, Issue 11
Review Article| November 01 1962

Crack Propagation: The Results of a Test Programme Based on a Gust Spectrum with Variable Amplitude Loading

;
J. Schijve
Nationaal Lucht‐ en Ruimtcvaartlaboratorium (National Aero‐and Astronautical Research Institute), Amsterdam, Holland.
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D. Broek
Nationaal Lucht‐ en Ruimtcvaartlaboratorium (National Aero‐and Astronautical Research Institute), Amsterdam, Holland.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1962
Aircraft Engineering (1962) 34 (11): 314–316.
https://doi.org/10.1108/eb033633

This paper deals with crack propagation under programme‐fatigue loading; the programme being derived from a gust spectrum. The validity of the Palmgren‐Miner rule for crack propagation has been studied and its usefulness for design purposes is discussed.

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© MCB UP Limited
1962
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