Coupled Navier–Stokes/Direct Simulation Monte Carlo Simulation of Multicomponent Mixture Plume Flows
Author:
Affiliation:
1. China Aerodynamics Research & Development Center, Hypervelocity Aerodynamics Institute, 621000 Mianyang, People’s Republic of China
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/10.2514/1.B34971
Reference49 articles.
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3. Analytical approximation for the flow from a nozzle into a vacuum.
4. Effect of nozzle boundary layers on rocket exhaust plumes.
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