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Critical stress of thin-walled cylinders in torsion /
A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small r...
| Clasificación: | Libro Electrónico |
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| Autores principales: | , , |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1344. |
| Temas: | |
| Acceso en línea: | Texto completo |
| Sumario: | A theoretical solution is given of the critical stress of thin-walled cylinders loaded in torsion. The results are presented in terms of a few simple formulas and curves which are applicable to a wide range of cylinder dimensions from very short cylinders of large radius to long cylinders of small radius. Theoretical results are found to be in somewhat better agreement with experimental results than previous theoretical work for the same range of cylinder dimensions. |
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| Notas: | "Langley Memorial Aeronautical Laboratory." Date of issue: June 1947. Report no. NACA TN No. 1344. |
| Descripción Física: | 1 online resource (21, [5] pages) : illustrations, tables |
| Bibliografía: | Includes bibliographical references (page 19) |
| ISBN: | 9781680156041 1680156047 |