Comparison of coupled radiative flow solutions with Project Fire II flight data-Reference-Cited by-同舟云学术

Comparison of coupled radiative flow solutions with Project Fire II flight data

Published:1995-10 Issue:4 Volume:9 Page:586-594
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Olynick David R.¹,Henline W. D.¹,Chambers Lin Hartung²,Candler G. V.³

Affiliation:

1. NASA Ames Research Center, Moffett Field, California 94035-1000

2. NASA Langley Research Center, Hampton, Virginia 23681-0001

3. University of Minnesota, Minneapolis, Minnesota 55455

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.712

Reference27 articles.

1. 2Candler, G. V. "The Computation of Weakly Ionized Hypersonic Flows in Chemical Nonequilibrium," Ph.D. Dissertation,Stanford Univ., Stanford, CA, June 1988.

2. Coupled radiation effects in thermochemical nonequilibrium shock-capturing flowfield calculations

3. 4Cornette, E. S. "Forebody Temperatures and Calorimeter Heating Rates Measured During Project Fire II Reentry at 11.35 km/s," NASA TM X-1305, Nov.1966.

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