Asymptotic convergence of higher-order accurate panel methods
Author:
Affiliation:
1. National Aerospace Laboratory NLR, Amsterdam, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45278
Reference13 articles.
1. Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex Configurations
2. 4Botta, E.F.F. "Calculation of Potential Flow Around Bodies," Ph.D. Thesis,University of Groningen, The Netherlands, 1978.
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