Flapping-Wing Fluid–Structural Interaction Analysis Using Corotational Triangular Planar Structural Element
Author:
Affiliation:
1. Seoul National University, Seoul 08826, Republic of Korea
2. Korea Aerospace Research Institute, Daejeon 34133, Republic of Korea
3. Inha University, Incheon 22212, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054567
Reference30 articles.
1. ShyyW.LianY.TangJ.ViieruD.LiuH., Aerodynamics of Low Reynolds Number Flyers, Chapter 4, Flapping-Wing Aerodynamics, Cambridge Univ. Press, New York, 2007, pp. 101–158.
2. A unified co-rotational framework for solids, shells and beams
3. A unified formulation of small-strain corotational finite elements: I. Theory
4. An Element Independent Corotational Procedure for the Treatment of Large Rotations
5. Flapping Wing CFD/CSD Aeroelastic Formulation Based on a Co-rotational Shell Finite Element
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