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...

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Bibliographic Details
Main Author: Ebner, H., (Author)
Corporate Author: United States. National Advisory Commitee for Aeronautics.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, [1937]
Series: Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 838.
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ISBN: 9781680156560
168015656X
Physical Description: 1 online resource (51 pages, 9 unnumbered pages) : illustrations

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Summary: 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.
Item Description: "September 1937."
NACA TM No. 838.
Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics.
Bibliography: Includes bibliographical references.
ISBN: 9781680156560
168015656X
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty