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Some Simple Solutions for Buckling Loads of Thin and Moderately Thick Cylindrical Shells and Panels Made of Laminated Composite Material
Geier, B. and Singh, G. (1997) Some Simple Solutions for Buckling Loads of Thin and Moderately Thick Cylindrical Shells and Panels Made of Laminated Composite Material. Aerospace Science and Technology, Vol. 1 (1), pp. 47-63.
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| Document Type: | Article | ||||||
|---|---|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=1999, | ||||||
| Title: | Some Simple Solutions for Buckling Loads of Thin and Moderately Thick Cylindrical Shells and Panels Made of Laminated Composite Material | ||||||
| Authors: |
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| Date: | 1997 | ||||||
| Journal or Publication Title: | Aerospace Science and Technology | ||||||
| Refereed publication: | Yes | ||||||
| In ISI Web of Science: | Yes | ||||||
| Volume: | Vol. 1 | ||||||
| Page Range: | pp. 47-63 | ||||||
| Status: | Published | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | no assignment | ||||||
| HGF - Program Themes: | no assignment | ||||||
| DLR - Research area: | Aeronautics | ||||||
| DLR - Program: | no assignment | ||||||
| DLR - Research theme (Project): | UNSPECIFIED | ||||||
| Location: | Braunschweig | ||||||
| Institutes and Institutions: | Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik | ||||||
| Deposited By: | elib DLR-Beauftragter | ||||||
| Deposited On: | 16 Sep 2005 | ||||||
| Last Modified: | 14 Jan 2010 15:32 |
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