Cargando…
A Method of calculating the compressive strength of Z-stiffened panels that develop local instability /
A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, a...
| 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. 1482. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_ocn919093676 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d | ||
| 007 | cr cnu---unuuu | ||
| 008 | 150824s1947 dcuad obt f000 0 eng d | ||
| 040 | |a KNOVL |b eng |e rda |e pn |c KNOVL |d ZCU |d UAB |d DKU |d OCLCQ |d CEF |d RRP |d YOU |d S2H |d OCLCO |d COP |d OCLCO |d OCLCQ |d UPM |d OCLCQ |d OCLCO | ||
| 020 | |a 9781680156102 |q (electronic bk.) | ||
| 020 | |a 1680156101 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856592145 | |
| 035 | |a (OCoLC)919093676 | ||
| 050 | 4 | |a TA660.P6 | |
| 082 | 0 | 4 | |a 624.17765 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:6/1482 | |
| 049 | |a UAMI | ||
| 100 | 1 | |a Gallaher, George L., |e author. | |
| 245 | 1 | 2 | |a A Method of calculating the compressive strength of Z-stiffened panels that develop local instability / |c by George L. Gallaher and Rolla B. Boughan. |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1947. | |
| 300 | |a 1 online resource (15 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 number 1482 | |
| 500 | |a "November 1947." | ||
| 500 | |a NACA TN No. 1482. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, as well as within, the elastic range. For stresses above three-fourths the compressive yield stress the method can be used for the approximate determination of the average compressive stress at maximum load. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Mathematical analysis. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Analyse mathématique. | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast | |
| 650 | 7 | |a Mathematical analysis |2 fast | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 700 | 1 | |a Boughan, Rolla B. | |
| 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 Gallaher, George L. |t Method of calculating the compressive strength of Z-stiffened panels that develop local instability |w (OCoLC)656605606 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v no. 1482. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpMCCSZSPU/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||