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Critical-stress of thin-walled cylinders in axial compression /
Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of nondimensional parameters of small-deflection theory and are compared with theoretical curves derived for the buckling of cylinders with simply sup...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , , |
| Autores Corporativos: | , |
| 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) ;
1343. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 088 | |a NACA-TN-1343 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Batdorf, S. B., |e author. | |
| 245 | 1 | 0 | |a Critical-stress of thin-walled cylinders in axial compression / |c by S.B. Batdorf, Murry Schildcrout, and Manuel Stein, Langley Memorial Aeronautical Laboratory, Langley Field, Va. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1947. | |
| 300 | |a 1 online resource (17 pages) : |b illustrations | ||
| 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 Technical note ; |v no. 1343 | |
| 500 | |a "Langley Memorial Aeronautical Laboratory." | ||
| 500 | |a Date of issue: June 1947. | ||
| 500 | |a Report no. NACA-TN-1343. | ||
| 504 | |a Includes bibliographical references (pages 15-16) | ||
| 583 | 1 | |a digitized |c 2011 |h University of North Texas |l committed to preserve |2 pda |5 TXdn. | |
| 588 | 0 | |a Print version record. | |
| 520 | |a Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of nondimensional parameters of small-deflection theory and are compared with theoretical curves derived for the buckling of cylinders with simply supported and clamped edges. An empirical equation is given for the buckling of cylinders having a length-radius ratio greater than about 0.75. The test data obtained from various sources follow the general trend of the theoretical curve for cylinders with clamped edges, agreeing closely with the theory in the case of short cylinders, but falling considerably below the theoretical results for long cylinders. -- |c Provided by publisher. | ||
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Thin-walled structures. | |
| 650 | 0 | |a Cylinders. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Structures à parois minces. | |
| 650 | 6 | |a Cylindres. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a cylinders (solids) |2 aat | |
| 650 | 7 | |a Thin-walled structures. |2 fast |0 (OCoLC)fst01150059 | |
| 650 | 7 | |a Cylinders. |2 fast |0 (OCoLC)fst00886041 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 700 | 1 | |a Schildcrout, Murry, |e author. | |
| 700 | 1 | |a Stein, Manuel, |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Batdorf, S.B. |t Critical-stress of thin-walled cylinders in axial compression |w (OCoLC)904438253 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 1343. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCSTWCACB/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||