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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| Main Author | |
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| Corporate Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
U.S. Government Printing Office,
1938.
|
| Series | Report (United States. National Advisory Committee for Aeronautics) ;
no. 636. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156409 1680156403 |
| Physical Description | 1 online resource (ii, 21 pages) : illustrations |
Cover
| 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. -- |
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| Bibliography: | Includes bibliographical references (page 21). |
| ISBN: | 9781680156409 1680156403 |
| Access: | Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty |
| Physical Description: | 1 online resource (ii, 21 pages) : illustrations |