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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...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| 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 |
MARC
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| 020 | |a 9781680156409 |q (electronic bk.) | ||
| 020 | |a 1680156403 |q (electronic bk.) | ||
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| 035 | |a (OCoLC)919150706 | ||
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| 086 | 0 | |a Y 3.N 21/5:5/636 | |
| 049 | |a UAMI | ||
| 100 | 1 | |a Kuhn, Paul. | |
| 245 | 1 | 0 | |a Approximate stress analysis of multistringer beams with shear deformation of the flanges / |c by Paul Kuhn. |
| 264 | 1 | |a Washington, D.C. : |b U.S. Government Printing Office, |c 1938. | |
| 300 | |a 1 online resource (ii, 21 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Report / National Advisory Committee for Aeronautics ; |v number 636 | |
| 504 | |a Includes bibliographical references (page 21). | ||
| 588 | 0 | |a Print version record. | |
| 520 | |a 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. -- |c Provided by publisher. | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Deformations (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 6 | |a Déformations (Mécanique) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a deformation. |2 aat | |
| 650 | 7 | |a Deformations (Mechanics) |2 fast | |
| 650 | 7 | |a Shear (Mechanics) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Kuhn, Paul. |t Approximate stress analysis of multistringer beams with shear deformation of the flanges |w (OCoLC)918949241 |
| 830 | 0 | |a Report (United States. National Advisory Committee for Aeronautics) ; |v no. 636. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpASAMBSD2/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||