Aeroelastic analysis of a flexible control surface with structural nonlinearity-Reference-Cited by-同舟云学术

Aeroelastic analysis of a flexible control surface with structural nonlinearity

Published:1995-07 Issue:4 Volume:32 Page:868-874
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Lee In¹,Kim Seung-Ho¹

Affiliation:

1. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.46803

Reference17 articles.

1. Flutter Analysis of Missile Control Surfaces Containing Structural Nonlinearities

2. 2Hauenstein, A. J., Laurenson, R. M., and Gubser, J. L. "Investigations of an Asymptotic Expansion Technique to Analyze Surfaces with Structural Nonlinearities," Final Rept. Air Force Office of Scientific Research (AFSOR) Contract F49620-84-C-0123.

3. Experimental and Theoretical Study of Nonlinear Flutter

4. An iterative procedure for nonlinear flutter analysis

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