Fatigue and Strength Loads Computed with Regression Equations Empirically Derived to Convert the Load Spectra to Design Values
Symposium; 19th, International Committee on Aeronautical Fatigue: ICAF 97; fatigue in new and ageing aircraft ; 1997 ; Edinburgh
International Committee on Aeronautical Fatigue: ICAF 97; fatigue in new and ageing aircraft ; 19 ; 943-954
1997-01-01
12 pages
Conference paper
English
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