The strength of shell bodies-- theory and practice:

The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell s...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Ebner, H. (VerfasserIn)
Format: Elektronisch E-Book
Sprache:English
Veröffentlicht: Washington, D.C National Advisory Commitee for Aeronautics 1937
Schriftenreihe:United States / National Advisory Committee for Aeronautics: Technical memorandum 838
Schlagworte:
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Zusammenfassung:The monocoque form of airplane construction has introduced a number of new problems to the stress calculator and the designer. The problems for the stress calculator fall into two groups: the determination of the stress condition (shell statics) and the determination of the failing strength (shell strength). The present report summarizes the most important theoretical and experimental results on this subject
Beschreibung:"September 1937. - Includes bibliographical references. - NACA TM No. 838. - Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics
Beschreibung:1 Online-Ressource (51 p., 9 unnumbered pages)
ISBN:9781680156560

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