Dynamic Aeroelastic Response of Aircraft Wings Modeled as Anisotropic Thin-Walled Beams-Reference-Cited by-同舟云学术

Dynamic Aeroelastic Response of Aircraft Wings Modeled as Anisotropic Thin-Walled Beams

Published:2003-05 Issue:3 Volume:40 Page:532-543
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Qin Zhanming¹,Librescu Liviu¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0219

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.3127

Reference27 articles.

1. Aeroelastic response of 2-D lifting surfaces to gust and arbitrary explosive loading signatures

2. 2Meirovitch, L., Principles and Techniques of Vibrations, Prentice-Hall, Upper SaddleRiver, NJ,1997, pp.189-194, 206-210.

3. 3Song, O. “Modeling and Response Analysis of Thin-Walled Beam Structures Constructed of Advanced Composite Materials,” Ph.D. Dissertation, Dept. of Engineering Science and Mechanics,Virginia PolytechnicInst.and State Univ., Blacksburg, VA,1990.

4. Behavior of Thin-Walled Beams Made of Advanced Composite Materials and Incorporating Non-Classical Effects

5. Free Vibration Of Anisotropic Composite Thin-Walled Beams Of Closed Cross-Section Contour

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