Assessment of the allowable design stresses and the corresponding fatigue life : Pres. at the International Committee on Aeronautical Fatigue Symposium Fatigue Design Procedures, Munich, Germany, 16.-18.6.1965
1965
11 S., 13 Bl. Abb
Book
Unknown
Local classification TIB: | fer 346 k a / fer 322 k / ver 706 k b |
Structural Testing as Related to Fatigue in Determining Allowable Static Stresses
SAE Technical Papers | 1963
|FATIGUE LIFE ENHANCEMENT OF TYPICAL AERONAUTICAL JOINTS BY MEANS OF ENGINEERED RESIDUAL STRESSES
British Library Conference Proceedings | 2022
|Aeronautical fatigue in the electronic era
TIBKAT | 1989
|