Equivalent-Plate Analysis for a Composite Wing with a Control Surface
Author:
Affiliation:
1. School of Mechanical and Aerospace Engineering, Seoul National University, Seoul 151-742, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032020
Reference23 articles.
1. Aeroelastic analysis of a flexible control surface with structural nonlinearity
2. Linear and Nonlinear Aeroelastic Analysis of Fighter-Type Wing with Control Surface
3. Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface
4. Static and Vibration Analyses of General Wing Structures Using Equivalent-Plate Models
5. Lessons from application of equivalent plate structural molding to an HSCT wing
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