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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. --
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Approximate stress analysis of multistringer beams with shear deformation of the flanges
1938, U.S. Government Printing Office
in English
1680156403 9781680156409
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Includes bibliographical references (page 21).
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