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Experimental study of deformation and of effective width in axially loaded sheet-stringer panels /
The deformation of two sheet-stringer panels subjected to end compression under carefully controlled end conditions was measured at a number of points and at a number of loads, most of which were above the load at which the sheet had begun to buckle. The two panels were identical except for the shee...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , , |
| Formato: | Documento de Gobierno Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington [D.C.] :
National Advisory Committee for Aeronautics,
1939.
|
| Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
684. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 086 | 0 | |a Y 3.N 21/5:6/684 | |
| 049 | |a UAMI | ||
| 100 | 1 | |a Ramberg, Walter, |e author. | |
| 245 | 1 | 0 | |a Experimental study of deformation and of effective width in axially loaded sheet-stringer panels / |c by Walter Ramberg, Albert E. McPherson, and Sam Levy. |
| 264 | 1 | |a Washington [D.C.] : |b National Advisory Committee for Aeronautics, |c 1939. | |
| 300 | |a 1 online resource (60 pages, 47 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 note / National Advisory Committee for Aeronautics ; |v No. 684 | |
| 588 | 0 | |a Online resource, PDF version; title from title page (TRAIL, viewed October 25, 2021). | |
| 500 | |a "February 1939." | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (pages 55-59). | ||
| 520 | 3 | |a The deformation of two sheet-stringer panels subjected to end compression under carefully controlled end conditions was measured at a number of points and at a number of loads, most of which were above the load at which the sheet had begun to buckle. The two panels were identical except for the sheet, which was 0.070-inch 24ST Alclad for specimen 1 and 0.25-inch 24ST aluminum alloy for specimen 6. A technique was developed for attaching Tuckerman optical strain gages to the sheeet by the method of attachment. This technique was used to explore the strain distribution in the sheet at various loads. The twisting and the bending of the stringers were measured by means of pointers attached to the stringers. The shape of the buckles in the sheet of specimen 6 was recorded at two loads by means of plaster casts. | |
| 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 Aluminum alloys. | |
| 650 | 0 | |a Deformations (Mechanics) | |
| 650 | 0 | |a Buckling (Mechanics) | |
| 650 | 6 | |a Plaques (Ingénierie) | |
| 650 | 6 | |a Aluminium |x Alliages. | |
| 650 | 6 | |a Déformations (Mécanique) | |
| 650 | 6 | |a Flambage (Résistance des matériaux) | |
| 650 | 7 | |a aluminum alloy. |2 aat | |
| 650 | 7 | |a deformation. |2 aat | |
| 650 | 7 | |a buckling. |2 aat | |
| 650 | 7 | |a warping. |2 aat | |
| 650 | 7 | |a Aluminum alloys. |2 fast |0 (OCoLC)fst00806309 | |
| 650 | 7 | |a Buckling (Mechanics) |2 fast |0 (OCoLC)fst00840001 | |
| 650 | 7 | |a Deformations (Mechanics) |2 fast |0 (OCoLC)fst00889780 | |
| 650 | 7 | |a Plates (Engineering) |2 fast |0 (OCoLC)fst01066785 | |
| 700 | 1 | |a McPherson, Albert E., |e author. | |
| 700 | 1 | |a Levy, Sam, |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. | |
| 776 | 0 | 8 | |i Print version: |a Ramberg, Walter. |t Experimental study of deformation and of effective width in axially loaded sheet-stringer panels. |d Washington D.C. : National Advisory Committee for Aeronautics ; 1939 |w (OCoLC)646048220 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 684. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpESDEWAL2/toc |z Texto completo |
| 994 | |a 92 |b IZTAP | ||