Electron density reduction in re-entry plasma due to nitrogen atom removal
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5678
Reference2 articles.
1. A STREAMTUBE APPROXIMATION FOR CALCULATION OF REACTION RATES IN THE INVISCID FLOW FIELD OF HYPERSONIC OBJECTS
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