Accurate solutions for transonic viscous flow over finite wings
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1052
Reference26 articles.
1. %eese, J. E., and Agarwal, R. K. "Calculation of Axisymmetr;c Inlet Flowfield Using the Euler Equations, AIAA Paper No. 83-1853, July 1983.
2. 4Jameson, A., and Baker, T. J. "solution Hf the Euler Equations for Complex Configurations, AIAA Paper NO. 83-1929, July 1983.
3. 'Baker, T. J., Jameson, A., and Vermeland, R. E. "Three-Dimensional Euler Solutions with Grid Embedding,' AIAA Paper No. 85-121, Jan. 1985.
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