Effect of delamination on flutter of composite laminated plates
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === The effect of delamination on the flutter boundary of a delaminated rectangular plate was investigated by Finite Strip Method. Linear structural theory, quasi-steady supersonic aerodynamic theory and a moving together model were empolyed for the analysis. Th...
Main Authors: | Yueh-Feng Tsai, 蔡岳峯 |
---|---|
Other Authors: | Le-Chung Shiau |
Format: | Others |
Language: | zh-TW |
Published: |
2007
|
Online Access: | http://ndltd.ncl.edu.tw/handle/97531651141343030010 |
Similar Items
-
Delamination Effect on Flutter Axially Loaded Composite Laminated Beam-Plates
by: Yuan-Shih Chen, et al.
Published: (1993) -
The effect of internal delamination on unsymmetric laminated composite plates
by: Palmer, David W.
Published: (2006) -
Finite Element Analysis of Flutter of Delaminated Beam-Plates
by: Shih-Yao Kuo, et al.
Published: (1995) -
Delamination of Composite Laminate Plate by Sliding Load Mode
by: Kormaníková Eva
Published: (2017-06-01) -
Analysis Of Delaminations In Tapered And Stiffened Laminated Composite Plates
by: Vijayaraju, K
Published: (2012)