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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| Format: | Regierungsdokument E-Book |
| Sprache: | Englisch |
| Veröffentlicht: |
Washington, D.C.
National Advisory Committee for Aeronautics
1949
|
| Schriftenreihe: | Report (United States. National Advisory Committee for Aeronautics)
934 |
| Links: | https://app.knovel.com/hotlink/toc/id:kpRNSRPFRJ/recommendations-for-numerical?kpromoter=marc |
| Zusammenfassung: | 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. -- Provided by publisher. |
| Beschreibung: | "Polytechnic Institute of Brooklyn." Creation date: June 25, 1947. Report no. NACA-TR-934. |
| Umfang: | 1 Online-Ressource (29 Seiten) Illustrationen |
| ISBN: | 1680156462 9781680156461 |
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| 100 | 1 | |a Hoff, Nicholas J. |d 1906- | |
| 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 National Advisory Committee for Aeronautics |c 1949 | |
| 300 | |a 1 Online-Ressource (29 Seiten) |b Illustrationen | ||
| 336 | |b txt | ||
| 337 | |b c | ||
| 338 | |b cr | ||
| 490 | 1 | |a Report (United States. National Advisory Committee for Aeronautics) |v 934 | |
| 500 | |a "Polytechnic Institute of Brooklyn." | ||
| 500 | |a Creation date: June 25, 1947. | ||
| 500 | |a Report no. NACA-TR-934. | ||
| 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. -- Provided by publisher. | ||
| 700 | 1 | |a Libby, Paul A. | |
| 966 | 4 | 0 | |l DE-91 |p ZDB-10-ARA |q TUM_PDA_ARA |u https://app.knovel.com/hotlink/toc/id:kpRNSRPFRJ/recommendations-for-numerical?kpromoter=marc |3 Volltext |
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| id | ZDB-10-ARA-ocn919161696 |
| illustrated | Illustrated |
| indexdate | 2025-03-03T13:03:35Z |
| institution | BVB |
| isbn | 1680156462 9781680156461 |
| language | English |
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| physical | 1 Online-Ressource (29 Seiten) Illustrationen |
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| publishDate | 1949 |
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| publisher | National Advisory Committee for Aeronautics |
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| series2 | Report (United States. National Advisory Committee for Aeronautics) |
| spelling | Hoff, Nicholas J. 1906- Recommendations for numerical solution of reinforced-panel and fuselage-ring problems by N.J. Hoff and Paul A. Libby Washington, D.C. National Advisory Committee for Aeronautics 1949 1 Online-Ressource (29 Seiten) Illustrationen txt c cr Report (United States. National Advisory Committee for Aeronautics) 934 "Polytechnic Institute of Brooklyn." Creation date: June 25, 1947. Report no. NACA-TR-934. 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. -- Provided by publisher. Libby, Paul A. |
| spellingShingle | Hoff, Nicholas J. 1906- Recommendations for numerical solution of reinforced-panel and fuselage-ring problems |
| title | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems |
| title_auth | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems |
| title_exact_search | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems |
| title_full | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems by N.J. Hoff and Paul A. Libby |
| title_fullStr | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems by N.J. Hoff and Paul A. Libby |
| title_full_unstemmed | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems by N.J. Hoff and Paul A. Libby |
| title_short | Recommendations for numerical solution of reinforced-panel and fuselage-ring problems |
| title_sort | recommendations for numerical solution of reinforced panel and fuselage ring problems |
| work_keys_str_mv | AT hoffnicholasj recommendationsfornumericalsolutionofreinforcedpanelandfuselageringproblems AT libbypaula recommendationsfornumericalsolutionofreinforcedpanelandfuselageringproblems |