Flutter analysis of anisotropic panels with patched cracks-Reference-Cited by-同舟云学术

Flutter analysis of anisotropic panels with patched cracks

Published:1991-12 Issue:12 Volume:28 Page:899-907
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Lin Kuo-Jiun¹,Lu Pong-Jeu¹,Tarn Jiann-Quo¹

Affiliation:

1. National Cheng Kung University, Tainan, Taiwan, Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46115

Reference27 articles.

1. ^erette, R. M., and Permits, E. "Effects of Manufacturing and In-Service Defects on Composite Materials," Army Material and Mechanics Research Center, MS76-Z,1976, pp.123-136.

2. 2Hoffman, G. A., and Konishi, D. Y. "Characterization of Manufacturing Flaws in Graphite-Epoxy," Army Material and Mechanics Research Center, MS77-5, pp.5.1.1-5.1.1.3,1977.

3. Flutter analysis of thin cracked panels using the finite element method

4. Analysis of Composite-Reinforced Cutouts and Cracks

5. On the use of special crack tip elements in cracked elastic sheets

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