Low-density nozzle flow by the direct simulation Monte Carlo and continuum methods
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
2. University of Toledo, Toledo, Ohio 43606
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23841
Reference41 articles.
1. Rocket nozzle lip flow by direct simulation Monte Carlo method
2. Nozzle-lip effects on argon expansions into the plume backflow
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