Application of computational aerodynamics to airplane design
Author:
Affiliation:
1. Lockheed-California Company, Burbank California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44974
Reference31 articles.
1. Rizzi A and Eriksson L E , 'Transfinite Mesh Generation and Damped Euler Equation Algorithm for Transonic Flow Around Wing Body Configurations AIAA Paper 81 0999 1981
2. 7Kandil O A Mook D T arid Nayfeh A H A Numerical Technique for Computing Subsonic Flow Past Three Dimensional Canard Wing Configurations with Edge Separations AIAA Paper 77 1,1977
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