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...
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| Main Authors | , |
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| Corporate Authors | , |
| Format | Electronic eBook |
| Language | English |
| Published |
Washington, D.C. :
U.S. Government Printing Office,
1949.
|
| Series | Report (United States. National Advisory Committee for Aeronautics) ;
no. 934. |
| Subjects | |
| Online Access | Full text |
| ISBN | 9781680156461 1680156462 |
| Physical Description | 1 online resource (29 pages) |
Cover
| Summary: | 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. -- |
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| Bibliography: | Includes bibliographical references (page 21). |
| ISBN: | 9781680156461 1680156462 |
| 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 (29 pages) |