Numerical study of gas-particle flow in a solid rocket nozzle
Author:
Affiliation:
1. National Cheng Kung University, Taiwan, Republic of China
2. Chung Shan Institute of Science and Technology, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9953
Reference21 articles.
1. Recent Advances in Gas-Particle Nozzle Flows
2. FLOW OF GAS-PARTICLE MIXTURES IN AXIALLY SYMMETRIC NOZZLES
3. Review—Numerical Models for Dilute Gas-Particle Flows
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