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Approximate stress analysis of multistringer beams with shear deformation of the flanges /

The problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Kuhn, Paul
Autores Corporativos: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : U.S. Government Printing Office, 1938.
Colección:Report (United States. National Advisory Committee for Aeronautics) ; no. 636.
Temas:
Acceso en línea:Texto completo
Descripción
Sumario:The problem of the skin-stringer combinations used as axially loaded panels or as covers for box beams is considered from the point of view of the practical stress analyst. By a simple substitution the problem is reduced to the problem of the single-stringer structure, which has been treated in NACA Report no. 608. The method of making this substitution is essentially empirical; in order to justify it, comparisons are shown between calculations and strain-gage tests of three beams tested by the author and of one compression panel and three beams tested and reported elsewhere. --
Descripción Física:1 online resource (ii, 21 pages) : illustrations
Bibliografía:Includes bibliographical references (page 21).
ISBN:9781680156409
1680156403