A Joint Computational Fluid Dynamics and Experimental Fluid Dynamics Test Program
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-877
Reference14 articles.
1. Development of a Low Cost, Rapid Prototype, Lambda Wing-Body Wind Tunnel Model
2. Cobalt: A parallel, implicit, unstructured Euler/Navier–Stokes solver
3. Recent experience with different methods of drag prediction
4. Use of pressure sensitive paints in low speed flows
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