Ultimate strength analysis of aircraft structures
- 1 May 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 7 (3) , 205-210
- https://doi.org/10.2514/3.44147
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Development of Fatigue Loading Spectra for Testing Aircraft Components and StructuresPublished by ASTM International ,1960
- Statistics of ExtremesPublished by Columbia University Press ,1958
- Safety and the Probability of Structural FailureTransactions of the American Society of Civil Engineers, 1956