Development of a Particle-Particle Hybrid Scheme based on ESBGK and DSMC Methods to Simulate Multi-scale Transitional Flows-Reference-Cited by-同舟云学术

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Development of a Particle-Particle Hybrid Scheme based on ESBGK and DSMC Methods to Simulate Multi-scale Transitional Flows

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Kumar Rakesh¹,Titov Evgeny¹,Levin Deborah¹

Affiliation:

1. Pennsylvania State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-625

Reference48 articles.

1. Examination of a Collision-Limiter Direct Simulation Monte Carlo Method for Micropropulsion Applications

2. 2Burch, B. "Effect of Contamination on Spacecraft Surfaces Exposed to Rocket Exhausts," Arnold Engineering Development Center, Technical Report, AEDC-TR-68-3,1968.

3. Characteristics of micronozzle gas flows

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