Velocity-Slip and Temperature-Jump Effects in Near-Continuum Hypersonic Flows
Author:
Affiliation:
1. University of Minnesota, Twin Cities, MN 55414
Funder
Air Force Office of Scientific Research
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059890
Reference52 articles.
1. GökçenT.MacCormackR.ChapmanD. R. “Computational Fluid Dynamics Near the Continuum Limit,” AIAA Paper 1987-1115, 1987.
2. Nonequilibrium Gas Dynamics and Molecular Simulation
3. Measurements in Regions of Low Density Laminar Shock Wave/Boundary Layer Interaction in Hypervelocity Flows and Comparison with Navier-Stokes Predictions.
4. Numerical Investigation of Unsteady Heat Transfer on a Double Wedge Geometry in Hypervelocity Flows
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