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The strength and stiffness of shear webs with and without lightening holes /
Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1942]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L402. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 003 | OCoLC | ||
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| 008 | 150825s1942 dcua obt f000 0 eng d | ||
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| 020 | |a 9781680156539 |q (electronic bk.) | ||
| 020 | |a 1680156535 |q (electronic bk.) | ||
| 029 | 1 | |a GBVCP |b 856592331 | |
| 035 | |a (OCoLC)919163322 | ||
| 050 | 4 | |a TA480.A6 | |
| 082 | 0 | 4 | |a 620.186 |2 23 |
| 086 | 0 | |a Y 3.N 21/5:11/L402 | |
| 088 | |a NACA WR 402 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Kuhn, Paul, |e author. | |
| 245 | 1 | 4 | |a The strength and stiffness of shear webs with and without lightening holes / |c Paul Kuhn. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 264 | 1 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1942] | |
| 300 | |a 1 online resource (29 pages, 15 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 Wartime Report / National Advisory Committee for Aeronautics ; |v number L402 | |
| 500 | |a NACA Wartime Report L-402. | ||
| 500 | |a Originally issued as NACA as an Advance Restricted Report (June 1942). | ||
| 500 | |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular and had either flanged edges or beaded edges, the specimens with flanged edges constituting by far the largest test group. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Holes. | |
| 650 | 0 | |a Shear (Mechanics) | |
| 650 | 0 | |a Strength of materials. | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Monocoque construction. | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Trous. | |
| 650 | 6 | |a Cisaillement (Mécanique) | |
| 650 | 6 | |a Résistance des matériaux. | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Tableaux, graphiques, etc. | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a shear stress. |2 aat | |
| 650 | 7 | |a strength of materials. |2 aat | |
| 650 | 7 | |a stress. |2 aat | |
| 650 | 7 | |a strain. |2 aat | |
| 650 | 7 | |a diagrams. |2 aat | |
| 650 | 7 | |a Aluminum alloys |2 fast | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast | |
| 650 | 7 | |a Holes |2 fast | |
| 650 | 7 | |a Monocoque construction |2 fast | |
| 650 | 7 | |a Shear (Mechanics) |2 fast | |
| 650 | 7 | |a Strains and stresses |2 fast | |
| 650 | 7 | |a Strength of materials |2 fast | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Kuhn, Paul. |t Strength and stiffness of shear webs with and without lightening holes |w (OCoLC)707923695 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L402. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpSSSWLHND/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||