An approximate inviscid radiating flow field analysis for outer planet entry probes
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-189
Reference30 articles.
1. 'Sutton, K. "Characteristicsof Coupled Nongray Radiating Gas Flows With Ablation Product Effects About Blunt Bodies During Planetary Entries," Ph.D Thesis, Department of Mechanical and Aerospace Engineering,Xorth Carolina State University, Raleigh, North Carolina,1975.
2. An approximate inviscid radiating flow-field analysis for sphere-cone Venusian entry vehicles
3. Inviscid hypersonic flow past smooth symmetric bodies
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