THE VISCOUS, RADIATING SHOCK LAYER ABOUT A BLUNT BODY
Author:
Affiliation:
1. LOCKHEED AIRCRAFT CORPORATION, PALO ALTO, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1964-1307
Reference27 articles.
1. The Effect of Thermal Radiation on the Inviscid Hypersonic Flow Over a Blunt Body
2. Dynamics of a dissociating gas Part I Equilibrium flow
3. The coupling of radiation and convection in detached shock layers
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. An approximate analysis of thermal conduction and radiative transport in the stagnation-point shock layer.;AIAA Journal;1966-03
2. Convective heat exchange in a radiating gas;Fluid Dynamics;1966
3. Shock-tube studies of equilibrium air radiation;AIAA Journal;1965-06
4. REENTRY HEATING AND THERMAL PROTECTION OF A MARS-MISSION EARTH-REENTRY MODULE;Entry Technology Conference;1964-08-16
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