Singa Rao, K. ; Venkateswara Rao, G. (1980) Large amplitude supersonic flutter of panels with ends elastically restrained against rotation Computers & Structures, 11 (3). pp. 197-201. ISSN 0045-7949
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Official URL: http://www.sciencedirect.com/science/article/pii/0...
Related URL: http://dx.doi.org/10.1016/0045-7949(80)90159-5
Abstract
Nonlinear supersonic flutter of panels is studied for end conditions of simply supported, clamped and partial restrained against rotation by a unified approach. The effects of large deflection and inplane forces on flutter boundary is included. Based on convergence study an eight element solution is given for all the results presented.
Item Type: | Article |
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Source: | Copyright of this article belongs to Elsevier Science. |
ID Code: | 53724 |
Deposited On: | 09 Aug 2011 11:04 |
Last Modified: | 09 Aug 2011 11:04 |
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