Nonlinear Aeroelastic Computation of a Wing/Pylon/Finned-Store Using Parallel Computing
Author:
Affiliation:
1. GyeongSang National University, Jinju 660-701, Republic of Korea
2. Korea Aerospace Research Institute, Taejon 305-333, Republic of Korea
3. 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/10.2514/1.11011
Reference33 articles.
1. Nonlinear transonic flutter analysis
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4. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method
5. Wing flutter boundary prediction using unsteady Euler aerodynamic method
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