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Critical combinations of torsion and direct axial stress for thin-walled cylinders /
A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical c...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autor Corporativo: | |
| Otros Autores: | , |
| 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. 1345. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 088 | |a NACA-TN-1345 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Batdorf, S. B., |e author. | |
| 245 | 1 | 0 | |a Critical combinations of torsion and direct axial stress for thin-walled cylinders / |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 (28, [8] 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. 1345 | |
| 500 | |a "Langley Memorial Aeronautical Laboratory." | ||
| 500 | |a Date of issue: June 1947. | ||
| 500 | |a Report no. NACA TN No. 1345. | ||
| 504 | |a Includes bibliographical references (page 25) | ||
| 520 | 3 | |a A theoretical solution is presented for the determination of the combinations of direct axial stress and torsion which cause thin-walled cylinders with either simply supported or clamped edges to buckle. This theoretical solution is used in conjunction with available test data to develop empirical curves and formulas for use in design. Comparisons are made with theoretical and empirical solutions obtained in other investigations. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Shells (Engineering) | |
| 650 | 0 | |a Thin-walled structures. | |
| 650 | 0 | |a Cylinders. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Torsion. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 6 | |a Coques (Ingénierie) | |
| 650 | 6 | |a Structures à parois minces. | |
| 650 | 6 | |a Cylindres. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Torsion (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 7 | |a shell structures. |2 aat | |
| 650 | 7 | |a cylinders (solids) |2 aat | |
| 650 | 7 | |a torsional stress. |2 aat | |
| 650 | 7 | |a Thin-walled structures. |2 fast |0 (OCoLC)fst01150059 | |
| 650 | 7 | |a Shells (Engineering) |2 fast |0 (OCoLC)fst01115734 | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast |0 (OCoLC)fst00840001 | |
| 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. | |
| 700 | 1 | |a Schildcrout, Murry. | |
| 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 combinations of torsion and direct axial stress for thin-walled cylinders. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1947 |w (OCoLC)652531421 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1345. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCCTDASTT/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||