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Critical combinations of shear and direct axial stress for curved rectangular panels /
A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.
| 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,
1949.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1928. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 008 | 150724s1949 ohua obt f000 0 eng d | ||
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| 020 | |a 9781680156164 |q (electronic bk.) | ||
| 020 | |a 1680156160 |q (electronic bk.) | ||
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| 035 | |a (OCoLC)914328363 |z (OCoLC)951667867 | ||
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| 086 | 0 | |a Y 3.N 21/5:6/1928 | |
| 088 | |a NACA-TN-1928 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Schildcrout, Murry. | |
| 245 | 1 | 0 | |a Critical combinations of shear and direct axial stress for curved rectangular panels / |c Murry Schildcrout and Manuel Stein. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1949. | ||
| 300 | |a 1 online resource (29 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 National Advisory Committee for Aeronautics ; |v no. 1928 | |
| 500 | |a "August 1949." | ||
| 500 | |a NACA TN No. 1928. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios. | |
| 520 | 3 | |a Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semi-empirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Curvature. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Courbure. | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast |0 (OCoLC)fst00840001 | |
| 650 | 7 | |a Curvature. |2 fast |0 (OCoLC)fst00885436 | |
| 650 | 7 | |a Plates (Engineering) |2 fast |0 (OCoLC)fst01066785 | |
| 650 | 7 | |a Shear (Mechanics) |2 fast |0 (OCoLC)fst01115422 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 700 | 1 | |a Stein, Manuel. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 730 | 0 | |a Technical Report Archive & Image Library (TRAIL) | |
| 776 | 0 | 8 | |i Print version: |a Schildcrout, Murry. |t Critical combinations of shear and direct axial stress for curved rectangular panels. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1949 |w (OCoLC)660169956 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1928. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCCSDASC1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||