Crack Propagation: The Results of a Test Programme Based on a Gust Spectrum with Variable Amplitude Loading
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 November 1962
Abstract
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.
Citation
Schijve, J. and Broek, D. (1962), "Crack Propagation: The Results of a Test Programme Based on a Gust Spectrum with Variable Amplitude Loading", Aircraft Engineering and Aerospace Technology, Vol. 34 No. 11, pp. 314-316. https://doi.org/10.1108/eb033633
Publisher
:MCB UP Ltd
Copyright © 1962, MCB UP Limited