Measurements in Regions of Low Density Laminar Shock Wave/Boundary Layer Interaction in Hypervelocity Flows and Comparison with Navier-Stokes Predictions.
Author:
Affiliation:
1. Calspan-UB Research Center
2. Veridian Engineering
3. Imperial College of Science
4. University of Minnesota
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1131
Reference12 articles.
1. 00E+00 0.00E+00 2.00E-01 4.00E-01 6.00E-01 8.00E-01 1.00E+00 1.20E+00 1.40E+00 1.60E+00 1.80E+00 2.00E+00
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