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...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Washington D.C
National Advisory Committee for Aeronautics
1939
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Technical note
684 |
| Schlagworte: | |
| Zusammenfassung: | 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 |
| Beschreibung: | 1 Online-Ressource (60, [47] p) |
| ISBN: | 9781680156027 |
Internformat
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| 100 | 1 | |a Ramberg, Walter |e Verfasser |0 (DE-588)125388780 |4 aut | |
| 245 | 1 | 0 | |a Experimental study of deformation and of effective width in axially loaded sheet-stringer panels |c 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-Ressource (60, [47] p) | ||
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| 490 | 1 | |a United States / National Advisory Committee for Aeronautics: Technical note |v 684 | |
| 520 | 8 | |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 | |
| 650 | 4 | |a Aluminum alloys | |
| 650 | 4 | |a Deformation (Mechanics) | |
| 650 | 4 | |a Plates (Engineering) | |
| 650 | 4 | |a Buckling (Mechanics) | |
| 700 | 1 | |a MacPherson, Albert E. |e Sonstige |4 oth | |
| 700 | 1 | |a Levy, Sam |e Sonstige |4 oth | |
| 810 | 2 | |a National Advisory Committee for Aeronautics: Technical note |t United States |v 684 |w (DE-604)BV006652327 |9 684 | |
| 912 | |a ZDB-10-KNL |a ZDB-10-ARA | ||
| 943 | 1 | |a oai:aleph.bib-bvb.de:BVB01-029382318 | |
Datensatz im Suchindex
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| author | Ramberg, Walter |
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| id | DE-604.BV043973784 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-31T01:10:29Z |
| institution | BVB |
| isbn | 9781680156027 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029382318 |
| oclc_num | 968236032 |
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| owner_facet | DE-91 DE-BY-TUM |
| physical | 1 Online-Ressource (60, [47] p) |
| psigel | ZDB-10-KNL ZDB-10-ARA |
| publishDate | 1939 |
| publishDateSearch | 1939 |
| publishDateSort | 1939 |
| publisher | National Advisory Committee for Aeronautics |
| record_format | marc |
| series2 | United States / National Advisory Committee for Aeronautics: Technical note |
| spelling | Ramberg, Walter Verfasser (DE-588)125388780 aut Experimental study of deformation and of effective width in axially loaded sheet-stringer panels Walter Ramberg, Albert E. McPherson, and Sam Levy Washington D.C National Advisory Committee for Aeronautics 1939 1 Online-Ressource (60, [47] p) txt rdacontent c rdamedia cr rdacarrier United States / National Advisory Committee for Aeronautics: Technical note 684 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 Aluminum alloys Deformation (Mechanics) Plates (Engineering) Buckling (Mechanics) MacPherson, Albert E. Sonstige oth Levy, Sam Sonstige oth National Advisory Committee for Aeronautics: Technical note United States 684 (DE-604)BV006652327 684 |
| spellingShingle | Ramberg, Walter Experimental study of deformation and of effective width in axially loaded sheet-stringer panels Aluminum alloys Deformation (Mechanics) Plates (Engineering) Buckling (Mechanics) |
| title | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels |
| title_auth | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels |
| title_exact_search | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels |
| title_full | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels Walter Ramberg, Albert E. McPherson, and Sam Levy |
| title_fullStr | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels Walter Ramberg, Albert E. McPherson, and Sam Levy |
| title_full_unstemmed | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels Walter Ramberg, Albert E. McPherson, and Sam Levy |
| title_short | Experimental study of deformation and of effective width in axially loaded sheet-stringer panels |
| title_sort | experimental study of deformation and of effective width in axially loaded sheet stringer panels |
| topic | Aluminum alloys Deformation (Mechanics) Plates (Engineering) Buckling (Mechanics) |
| topic_facet | Aluminum alloys Deformation (Mechanics) Plates (Engineering) Buckling (Mechanics) |
| volume_link | (DE-604)BV006652327 |
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