Approximate stress analysis of multistringer beams with shear deformation of the flanges
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1938 - U.S. Government Printing Office, Washington, D.C, District of Columbia
Language
English
Word Count
5,250 words, Guess
Page Count
21 pages
Identifiers
- ISBN-101680156403
- ISBN-139781680156409
- OCLC Control Number919150706
- Open LibraryOL44477779M
Classifications
- DDC620.11245
- LCCTA417.7.S5
Description
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. --
Subjects
Series Statement
- Report / National Advisory Committee for Aeronautics -- number 636
- Report (United States. National Advisory Committee for Aeronautics) -- no. 636.
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