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Square plate with clamped edges under normal pressure producing large deflections /
A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, [D.C.] :
National Advisory Committee for Aeronautics,
1942.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
847. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | KNOVEL_ocn919151114 | ||
| 003 | OCoLC | ||
| 005 | 20231027140348.0 | ||
| 006 | m o d f | ||
| 007 | cr bn||||||||| | ||
| 008 | 150825s1942 dcua ob f000 0 eng c | ||
| 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 TRAAL |d S2H |d OCLCO |d GPO |d OCLCO |d OCL |d OCLCO | ||
| 019 | |a 1164733650 | ||
| 020 | |a 9781680156430 |q electronic bk. | ||
| 020 | |a 1680156438 |q electronic bk. | ||
| 029 | 1 | |a GBVCP |b 856592315 | |
| 035 | |a (OCoLC)919151114 |z (OCoLC)1164733650 | ||
| 042 | |a pcc | ||
| 050 | 4 | |a TL501 | |
| 082 | 0 | 4 | |a 629.4 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:6/847 | |
| 049 | |a UAMI | ||
| 100 | 1 | |a Levy, Samuel, |e author. | |
| 245 | 1 | 0 | |a Square plate with clamped edges under normal pressure producing large deflections / |c by Samuel Levy. |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1942. | |
| 300 | |a 1 online resource (25 pages, 5 unnumbered 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 notes / National Advisory Committee for Aeronautics ; |v no. 847 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed April 25, 2022). | ||
| 500 | |a "May 1942." | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (pages 17-18). | ||
| 520 | |a A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to 1.9 times the plate thickness. The shape of the deflected surface is given for low pressures and for the highest pressure considered. Convergence of solution is considered and it is estimated that the possible error is less than 2 percent. -- |c Provided by publisher. | ||
| 583 | 1 | |a digitized |c 2011 |h University of North Texas |l committed to preserve |2 pda |5 TXdn. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Loads (Mechanics) | |
| 650 | 0 | |a Aeronautics |x Research. | |
| 650 | 0 | |a Airplanes |x Design and construction. | |
| 650 | 0 | |a Strains and stresses |x Analysis. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Charges. | |
| 650 | 6 | |a Aéronautique |x Recherche. | |
| 650 | 6 | |a Avions |x Conception et construction. | |
| 650 | 6 | |a Contraintes (Mécanique) |x Analyse. | |
| 650 | 7 | |a Plates (Engineering) |2 fast | |
| 650 | 7 | |a Loads (Mechanics) |2 fast | |
| 650 | 7 | |a Aeronautics |x Research |2 fast | |
| 650 | 7 | |a Airplanes |x Design and construction |2 fast | |
| 650 | 7 | |a Strains and stresses |x Analysis |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 776 | 0 | 8 | |i Print version: |a Levy, Samuel. |t Square plate with clamped edges under normal pressure producing large deflections. |d Washington D.C. : National Advisory Committee for Aeronautics, 1942 |w (OCoLC)646863696 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 847. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpSPCENPP1/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||