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The effect of internal pressure on the buckling stress of thin-walled circular cylinders under torsion /
The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a si...
| Clasificación: | Libro Electrónico |
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| Autores principales: | , , |
| Autores Corporativos: | , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1944]
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| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L67. |
| Temas: | |
| Acceso en línea: | Texto completo |
| Sumario: | The results of a series of tests to determine the effect of internal pressure on the buckling load of a thin cylinder under an applied torque indicated that internal pressure raises the shear buckling stress. The experimental results were analyzed with the aid of previously developed theory and a simple interaction formula was derived. |
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| Notas: | NACA Wartime Report L-67. Originally issued as NACA as Advance Restricted Report L4E27 (May 1944). Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. |
| Descripción Física: | 1 online resource (15 pages, 9 unnumbered pages) : illustrations |
| Bibliografía: | Includes bibliographical references. |
| ISBN: | 9781680156362 1680156365 |