Tension fields in originally curved, thin sheets during shearing stresses:
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders wit...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Washington, D.C
National Advisory Commitee for Aeronautics
1935
|
| Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Technical memorandum
774 |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Zusammenfassung: | The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings |
| Beschreibung: | "August 1935. - Includes bibliographical references. - NACA TM No. 774. - Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics. - Use copy Restrictions unspecified star MiAaHDL |
| Beschreibung: | 1 Online-Ressource (11 p., 2 unnumbered pages) |
| ISBN: | 9781680156577 |
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| 245 | 1 | 0 | |a Tension fields in originally curved, thin sheets during shearing stresses |c H. Wagner and W. Ballerstedt |
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| 490 | 1 | |a United States / National Advisory Committee for Aeronautics: Technical memorandum |v 774 | |
| 500 | |a "August 1935. - Includes bibliographical references. - NACA TM No. 774. - Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics. - Use copy Restrictions unspecified star MiAaHDL | ||
| 520 | 8 | |a The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings | |
| 650 | 4 | |a Strains and stresses | |
| 650 | 4 | |a Shells (Engineering) | |
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| id | DE-604.BV043976675 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-31T01:10:29Z |
| institution | BVB |
| isbn | 9781680156577 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-029385149 |
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| physical | 1 Online-Ressource (11 p., 2 unnumbered pages) |
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| publishDate | 1935 |
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| series2 | United States / National Advisory Committee for Aeronautics: Technical memorandum |
| spelling | Wagner, H. Verfasser aut Tension fields in originally curved, thin sheets during shearing stresses H. Wagner and W. Ballerstedt Washington, D.C National Advisory Commitee for Aeronautics 1935 1 Online-Ressource (11 p., 2 unnumbered pages) txt rdacontent c rdamedia cr rdacarrier United States / National Advisory Committee for Aeronautics: Technical memorandum 774 "August 1935. - Includes bibliographical references. - NACA TM No. 774. - Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics. - Use copy Restrictions unspecified star MiAaHDL The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings Strains and stresses Shells (Engineering) Shear (Mechanics) Thin-walled structures Curvature Ballerstedt, W. Sonstige oth National Advisory Committee for Aeronautics: Technical memorandum United States 774 (DE-604)BV008909669 774 http://app.knovel.com/hotlink/toc/id:kpTFOCTSS1/tension_fields_in_originally_curved_thin_sheets_during_shearing_stresses_naca_technical_memorandums_774 Volltext |
| spellingShingle | Wagner, H. Tension fields in originally curved, thin sheets during shearing stresses Strains and stresses Shells (Engineering) Shear (Mechanics) Thin-walled structures Curvature |
| title | Tension fields in originally curved, thin sheets during shearing stresses |
| title_auth | Tension fields in originally curved, thin sheets during shearing stresses |
| title_exact_search | Tension fields in originally curved, thin sheets during shearing stresses |
| title_full | Tension fields in originally curved, thin sheets during shearing stresses H. Wagner and W. Ballerstedt |
| title_fullStr | Tension fields in originally curved, thin sheets during shearing stresses H. Wagner and W. Ballerstedt |
| title_full_unstemmed | Tension fields in originally curved, thin sheets during shearing stresses H. Wagner and W. Ballerstedt |
| title_short | Tension fields in originally curved, thin sheets during shearing stresses |
| title_sort | tension fields in originally curved thin sheets during shearing stresses |
| topic | Strains and stresses Shells (Engineering) Shear (Mechanics) Thin-walled structures Curvature |
| topic_facet | Strains and stresses Shells (Engineering) Shear (Mechanics) Thin-walled structures Curvature |
| url | http://app.knovel.com/hotlink/toc/id:kpTFOCTSS1/tension_fields_in_originally_curved_thin_sheets_during_shearing_stresses_naca_technical_memorandums_774 |
| volume_link | (DE-604)BV008909669 |
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