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Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels /
Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given.
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Autores Corporativos: | , |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1944]
|
| Colección: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L204. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 008 | 150727s1944 dcua obt f000 0 eng d | ||
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| 050 | 4 | |a TA480.A6 | |
| 082 | 0 | 4 | |a 620.186 |2 23 |
| 088 | |a NACA WR L204 | ||
| 088 | |a NACA ARR L4H29 | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Boughan, Rolla B. | |
| 245 | 1 | 0 | |a Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels / |c Rolla B. Boughan and George W. Baab. |
| 246 | 3 | |a NACA Wartime Reports. Series L. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1944] | ||
| 300 | |a 1 online resource (8, [6] 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 no. L204 | |
| 500 | |a NACA Wartime Report L-204. | ||
| 500 | |a Originally issued as NACA as Advance Restricted Report L4H29 (August 1944). | ||
| 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 compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given. | |
| 588 | 0 | |a Print version record. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Aluminum alloys. | |
| 650 | 0 | |a Plates (Engineering) | |
| 650 | 0 | |a Strains and stresses. | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 0 | |a Airplanes |x Materials. | |
| 650 | 0 | |a Charts, diagrams, etc. | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Contraintes (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 6 | |a Avions |x Matériaux. | |
| 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 buckling. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a diagrams. |2 aat | |
| 650 | 7 | |a Airplanes |x Materials. |2 fast |0 (OCoLC)fst00803290 | |
| 650 | 7 | |a Aluminum alloys. |2 fast |0 (OCoLC)fst00806309 | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast |0 (OCoLC)fst00840001 | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545 | |
| 650 | 7 | |a Plates (Engineering) |2 fast |0 (OCoLC)fst01066785 | |
| 650 | 7 | |a Strains and stresses. |2 fast |0 (OCoLC)fst01134288 | |
| 700 | 1 | |a Baab, George W. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. | |
| 710 | 2 | |a Langley Aeronautical Laboratory. | |
| 776 | 0 | 8 | |i Print version: |a Boughan, Rolla B. |t Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels. |d Washington, D.C. : National Advisory Committee for Aeronautics, [1944] |w (OCoLC)706693060 |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. L204. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCCCCSLI2/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||