Efficient algorithm for unsteady transonic aerodynamics of low-aspect-ratio wings
Author:
Affiliation:
1. Informatics General Corporation, Palo Alto, California
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45107
Reference14 articles.
1. An implicit conservative algorithm for steady and unsteady three-dimensional transonic potential flows
2. Nonlinear transonic flutter analysis
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2. Transonic flow potential method development at Ames research center;Computers & Fluids;2009-03
3. Transonic Nonlinear Aeroelastic Analysis of Aircraft Tail Wings Using Multiblock Approach;Journal of Aircraft;2008-07
4. Transonic and supersonic flutter characteristics of a wing-box model with tip stores;19th AIAA Applied Aerodynamics Conference;2001-06-11
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