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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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Ebner, H. (Autor)
Autor Corporativo: United States. National Advisory Commitee for Aeronautics
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Commitee for Aeronautics, [1937]
Colección:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 838.
Temas:
Monocoque construction.
Shells (Engineering)
Strains and stresses.
Mathematics.
Coques (Ingénierie)
Contraintes (Mécanique)
Mathématiques.
shell structures.
stress.
strain.
applied mathematics.
mathematics.
Mathematics
Monocoque construction
Strains and stresses
Acceso en línea:Texto completo
Descripción
Sumario: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.
Notas:"September 1937."
NACA TM No. 838.
Translated from Luftfahrtforschung. Vol. 14, No. 3, March 20, 1937, by the National Advisory Commitee for Aeronautics.
Descripción Física:1 online resource (51 pages, 9 unnumbered pages) : illustrations
Bibliografía:Includes bibliographical references.
ISBN:9781680156560
168015656X

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