Numerical Analysis of Carbon Dioxide Flowfield in Expansion-Tube
Author:
Affiliation:
1. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3221
Reference44 articles.
1. A summary review of the scientific findings of the Mariner Venus mission
2. The Pioneer Venus Spacecraft Program
3. Analysis of the Heat-Shield Experiment on the Pioneer-Venus Entry Probes
4. Venera 4 Probes Atmosphere of Venus
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3. Evaluation of Hypervelocity Carbon Dioxide Blunt Body Experiments in an Expansion Tube Facility;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
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