Non-Linear Impulse Methods for Aeroelastic Simulations
Author:
Affiliation:
1. National University of Singapore
2. University of California
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4845
Reference35 articles.
1. Flutter Simulation and Prediction Via Identification of Non-Linear Impulse Response
2. Computation of Unsteady Transonic Flows by the Indicial Method
3. Parallel Computation of Wing Flutter with a Coupled Navier-Stokes/CSD Method
4. Unsteady Flow Calculations with a Parallel Multiblock Moving Mesh Algorithm
5. Calculation of Wing Flutter by a Coupled Fluid-Structure Method
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