Aileron Reversal of Nonuniform and Swept Composite Aircraft Wings-Reference-Cited by-同舟云学术

Aileron Reversal of Nonuniform and Swept Composite Aircraft Wings

Published:2013-05 Issue:3 Volume:50 Page:681-693
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Kim Keun-Taek¹,Song Ohseop²

Affiliation:

1. Aerodynamics and Structures Department, Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea

2. Mechanical Engineering Department, Chungnam National University, Daejeon 305-764, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031212

Reference25 articles.

1. Introduction to Structural Dynamics and Aeroelasticity

2. Solid Mechanics and Its Applications;Librescu L.,2006

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

4. QinZ. “Vibration and Aeroelasticity of Advanced Aircraft Wings Modeled as Thin-Walled Beams—Dynamics, Stability and Control,” Ph.D. Dissertation, Dept. of Engineering Science and Mechanics, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 2001.

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