Supersonic base-flow computation using higher-order closure turbulence models
Author:
Affiliation:
1. Chung Shan Institute of Science and Technology, Lung-Tan, Taiwan 325, Republic of China
2. National Tsing Hua University, Hsinchu, Taiwan 300, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26770
Reference22 articles.
1. Computations of supersonic flow over a missile afterbody containing an exhaust jet
2. Calculation of turbulent flow about missile afterbodies containing an exhaust jet
3. Comparison of algebraic turbulence models for afterbody flows with jet exhaust
4. Theoretical study of supersonic flow separation over a rearward facing step
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