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Recommendations for numerical solution of reinforced-panel and fuselage-ring problems /
Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. From the solution of these equations the stress distribution can be eas...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , |
| Autores Corporativos: | , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
U.S. Government Printing Office,
1949.
|
| Colección: | Report (United States. National Advisory Committee for Aeronautics) ;
no. 934. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Hoff, Nicholas J. |q (Nicholas John), |d 1906- |e author. | |
| 245 | 1 | 0 | |a Recommendations for numerical solution of reinforced-panel and fuselage-ring problems / |c by N.J. Hoff and Paul A. Libby. |
| 264 | 1 | |a Washington, D.C. : |b U.S. Government Printing Office, |c 1949. | |
| 300 | |a 1 online resource (29 pages) | ||
| 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 934 | |
| 504 | |a Includes bibliographical references (page 21). | ||
| 588 | 0 | |a Print version record. | |
| 520 | |a Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. From the solution of these equations the stress distribution can be easily determined. The method of systematic relaxations, the matrix-calculus method, and several other methods applicable in special cases are discussed. Definite recommendations are made for obtaining the solution of reinforced-panel problems which are generally designated as shear lag problems. The procedures recommended are demonstrated in the analysis of a number of panels. In the case of fuselage rings it is not possible to make definite recommendations for the solution of the equilibrium equations for all rings and loadings. -- |c Provided by publisher. | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Aeronautics |x Research. | |
| 650 | 0 | |a Airplanes |x Fuselage. | |
| 650 | 0 | |a Airplanes |x Design and construction. | |
| 650 | 6 | |a Aéronautique |x Recherche. | |
| 650 | 6 | |a Avions |x Fuselage. | |
| 650 | 6 | |a Avions |x Conception et construction. | |
| 650 | 7 | |a fuselages. |2 aat | |
| 650 | 7 | |a Aeronautics |x Research |2 fast | |
| 650 | 7 | |a Airplanes |x Design and construction |2 fast | |
| 650 | 7 | |a Airplanes |x Fuselage |2 fast | |
| 700 | 1 | |a Libby, Paul A., |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Polytechnic Institute of Brooklyn. | |
| 776 | 0 | 8 | |i Print version: |a Hoff, N.J. |t Recommendations for numerical solution of reinforced-panel and fuselage-ring problems |w (OCoLC)46869359 |
| 830 | 0 | |a Report (United States. National Advisory Committee for Aeronautics) ; |v no. 934. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpRNSRPFRJ/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||