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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Bibliographic Details
Main Author: Kuhn, Paul.
Corporate Authors: United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : U.S. Government Printing Office, 1938.
Series: Report (United States. National Advisory Committee for Aeronautics) ; no. 636.
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ISBN: 9781680156409
1680156403
Physical Description: 1 online resource (ii, 21 pages) : illustrations

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Summary: 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. --
Bibliography: Includes bibliographical references (page 21).
ISBN: 9781680156409
1680156403
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