Radiation effects in the stagnation region.
Author:
Affiliation:
1. Lockheed Palo Alto Research Laboratory, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3794
Reference16 articles.
1. Dynamics of a radiating gas by a differential approximation, with application to flow over a wavy wall
2. Traugott, S. C. "A differential approximation for radiative transfer with application to normal shock structure/7Martin Co. Kept. RR-34 (1962).
3. Heat Transfer by Simultaneous Conduction and Radiation in an Absorbing Medium
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1. Distribution of radiant thermal flux over the surface of a sphere for hypersonic flow of a nonviscous radiating gas past the sphere;Journal of Applied Mechanics and Technical Physics;1972-11
2. On stagnation-point conditions in non-equilibrium inviscid blunt-body flows;Journal of Fluid Mechanics;1970-08-17
3. RADIATING FLOWS DURING ENTRY INTO PLANETARY ATMOSPHERES;Propulsion Re-Entry Physics;1970
4. Radiant heat transfer in a spherically symmetric medium.;AIAA Journal;1968-07
5. Heat transfer—A review of current literature;International Journal of Heat and Mass Transfer;1968-02
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