TranAir and Euler computations of a generic fighter including comparisons with experimental data
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-263
Reference21 articles.
1. Xewsome. R.W. and Kandil. O.A. "Yortical Flow Aerodynanlics -Physical Aspects and Xumerical Sirnulation". AIAA Paper 87-0203. January 1987.
2. 'Stanhrook. A. and Squire,L. C'. *.Pos 5ihle Types of Flow at Swept Leading Edges", Xeronautical Ouarterlyvol. SY pt.1. pp.73-82. February 1961.
3. Powell, K. G. "Vortical Solutions of the Conical Euler Equations", PhD thesis,Massachusetts Institute of Technology, 1587.
4. 'Fujii. K. and Schiff,L. B."Numerical Simulation of Vortical Flows Over a Strake-Delta Wing". AIAA Paper 87-1229. 1987.
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