Simultaneous solution of the inviscid flow with a finite-difference boundary layer calculation
Author:
Affiliation:
1. U.S. Naval Postgraduate School, Monterey, CA; VirginiaPolytechnic Institute and State University, Blacksburg, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1274
Reference29 articles.
1. Since the ultimate objective is a simultaneous s o l u t i o n of t h e i n v i s c i d flow and boundary layer: a method based on the e a r l y simultaneous calculations was suggested in reference 9. I n t h i s approach, a line-relaxation technique was used f o r t h e i n v i s c i d flow, which was coupled d i r e c t l y t o an i n t e g r a l method f o r t h e boundary layer. Further examples of t h i s bas:tc approach are given i n References 10-14.
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