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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 |
|---|---|
| Autores principales: | , , |
| Autor Corporativo: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1344. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Batdorf, S. B., |e author. | |
| 245 | 1 | 0 | |a Critical stress of thin-walled cylinders in torsion / |c by S.B. Batdort, Manuel Stein and Murry Schildcrout. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1947. | |
| 300 | |a 1 online resource (21, [5] pages) : |b illustrations, tables | ||
| 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 National Advisory Committee for Aeronautics technical note ; |v no. 1344 | |
| 500 | |a "Langley Memorial Aeronautical Laboratory." | ||
| 500 | |a Date of issue: June 1947. | ||
| 500 | |a Report no. NACA TN No. 1344. | ||
| 504 | |a Includes bibliographical references (page 19) | ||
| 520 | 3 | |a 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. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Shells (Engineering) |x Thin-walled structures. | |
| 650 | 0 | |a Cylinders. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Torsion. | |
| 650 | 6 | |a Cylindres. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Torsion (Mécanique) | |
| 650 | 7 | |a cylinders (solids) |2 aat | |
| 650 | 7 | |a torsional stress. |2 aat | |
| 650 | 7 | |a Cylinders. |2 fast |0 (OCoLC)fst00886041 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 650 | 7 | |a Torsion. |2 fast |0 (OCoLC)fst01152860 | |
| 700 | 1 | |a Stein, Manuel, |e author. | |
| 700 | 1 | |a Schildcrout, Murry, |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Batdorf, S.B. |t Critical stress of thin-walled cylinders in torsion. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1947 |w (OCoLC)652531296 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1344. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCSTWCTN7/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||