Nonequilibrium, ionized, hypersonic flow over a blunt body at low Reynolds number
Author:
Affiliation:
1. Cornell Aeronautical Laboratory, Inc., Buffalo, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5883
Reference21 articles.
1. APPROXIMATE METHOD FOR HYPERSONIC NONEQUILIBRIUM BLUNT BODY AIRFLOWS
2. Prediction of the electron number density distribution in the laminar air boundary layer on sharp and blunt bodies
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