Results of test program, undertaken at Nat Aero and Astronautical Research Inst, Amsterdam, Holland, based on gust spectrum with variable amplitude loading; validity of Palmgren-Miner rule for crack propagation is studied and its usefulness for design purposes discussed.
Crack propagation
Aircraft Eng
Aircraft Engineering ; 34 , n 405
1962
3 pages
Article (Journal)
English
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Emerald Group Publishing | 1962
|NTRS | 1980
|NTRS | 1967
|NTRS | 1977
|Springer Verlag | 2017
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