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.
Crack Propagation
The Results of a Test Programme Based on a Gust Spectrum with Variable Amplitude Loading
Aircraft Engineering and Aerospace Technology ; 34 , 11 ; 314-316
1962-11-01
3 pages
Article (Journal)
Electronic Resource
English
Engineering Index Backfile | 1962
|NTRS | 1980
|NTRS | 1967
|NTRS | 1977
|Springer Verlag | 2017
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