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Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel, and rectangular-tube section /
Charts are presented for the calculation of the critical stress for local instability of columns with I-, Z-, channel, and rectangular-tube section. These charts are intended to replace the less complete charts published in NACA Technical Note No. 743. The values used in extending the charts are com...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1943]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L429. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 082 | 0 | 4 | |a 624.17725 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Kroll, W. D. | |
| 245 | 1 | 0 | |a Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel, and rectangular-tube section / |c W.D. Kroll, Gordon P. Fisher, and George J. Heimerl. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1943] | ||
| 300 | |a 1 online resource (18, [12] 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 Wartime Report / National Advisory Committee for Aeronautics ; |v no. L429 | |
| 500 | |a NACA Wartime Report L-429. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L3K04 (November 1943). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Charts are presented for the calculation of the critical stress for local instability of columns with I-, Z-, channel, and rectangular-tube section. These charts are intended to replace the less complete charts published in NACA Technical Note No. 743. The values used in extending the charts are computed by moment-distribution methods that give somewhat more accurate values than the energy method previously used and also make it possible to determine theoretically which element of the cross section is primarily responsible for instability. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Columns. | |
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Tubes. | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Tubes. | |
| 650 | 6 | |a Tableaux, graphiques, etc. | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a pipes (conduits) |2 aat | |
| 650 | 7 | |a diagrams. |2 aat | |
| 650 | 7 | |a Aluminum alloys. |2 fast |0 (OCoLC)fst00806309 | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545 | |
| 650 | 7 | |a Columns. |2 fast |0 (OCoLC)fst00868845 | |
| 650 | 7 | |a Loads (Mechanics) |2 fast |0 (OCoLC)fst01739107 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 650 | 7 | |a Tubes. |2 fast |0 (OCoLC)fst01158581 | |
| 700 | 1 | |a Fisher, Gordon P. | |
| 700 | 1 | |a Heimerl, George J. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Kroll, W.D. |t Charts for calculation of the critical stress for local instability of columns with I-, Z-, channel, and rectangular-tube section. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1943] |w (OCoLC)707938646 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L429. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCCCSLICF/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||