Upwind Navier-Stokes solutions for separated periodic flows
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-247
Reference28 articles.
1. 0 -0.8 t o 0.8 ref. 2, 3t=0.174
2. ir, 0 -0.6 t o 0.6 0"95 0.189 ) t o 0.196 0 0.3 200 thrn-layer 101x101 0.00056 FLAT PLATE
3. ref. 4, St=O. 164-0.172 ref. 4, St=0.153
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