Prediction of separated transonic wing flows with a non-equilibrium algebraic model
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. NASA, Ames Research Center, Moffett Field, CA
3. Vigyan Research Associates, Inc., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-558
Reference24 articles.
1. Workshop Compendium of Paper 87-1460, Jan. 1987. lransonic Airfoi I Results," AlAA C21 Coakley, T. J. "Numerical Simul;tion of
2. Viscous Transonic Airfoils Flows, AIAA Paper 87-0416, Jan. 1987. [31 Johnson, D. A, and King, L. S. "A
3. Solutions for Transonic Viscous Flow Over Finite. Wings," Journal of Aircraft, Vol.24, June 1987, pp.377-385.
4. Wing bunted in a Tunnel," AIAA Paper 88-0102, Jan. 1988.
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