Application of a higher order panel method to realistic supersonic configurations
Author:
Affiliation:
1. Boeing Aerospace Company, Seattle, Wash.
2. Mississippi State University, Miss.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44647
Reference21 articles.
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