Hypersonic Merged Stagnation Shock Layers Part 11: Cold Wall Case
Author:
Affiliation:
1. Marshall Space Flight Center, Huntsville, Ala.
2. Indian Institute of Technology, Kanpur, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49232
Reference16 articles.
1. Density Disturbance ahead of a Sphere in Rarefied Supersonic Flow
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3. Blunt-Body Heat Transfer at Hypersonic Speed and Low Reynolds Numbers
4. Measurements of Stagnation Point Heat Transfer at Low Reynolds Numbers
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1. Hypersonic Pressure, Skin-Friction and Heat Transfer Distributions On Space Vehicles: Three-Dimensional Bodies;AIAA Journal;2004-10
2. Hypersonic Pressure, Skin-Friction, and Heat Transfer Distributions On Space Vehicles: Planar Bodies;AIAA Journal;2004-10
3. Hypersonic rarefied flow and its solution over the stagnation region;28th Aerospace Sciences Meeting;1990-01-08
4. Chemical and thermal nonequilibrium heat transfer analysis for hypervelocity, low Reynolds number flow;20th Thermophysics Conference;1985-06-19
5. Slip Effects in Hypersonic Rarefied Flow;Rarefied Gas Dynamics, Parts I and II;1981-01-01
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