Study on Opposing Jet Simulation of Near Space Supersonic Vehicle Based on DSMC Method-Reference-Cited by-同舟云学术

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Study on Opposing Jet Simulation of Near Space Supersonic Vehicle Based on DSMC Method

Published:2022-08-16 Issue: Volume: Page:
ISSN:
Container-title:2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST)
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Author:

Shen Yi¹,Xu Xiao²,Zhang Jun¹,Zhang Zhaoming¹

Affiliation:

1. Ministry of Industry and Information Technology Nanjing University of Aeronautics and Astronautics,Key Laboratory of Unsteady Aerodynamics and Flow Control,Nanjing,China

2. Jiangsu University of Science and Technology(Zhangjiagang),School of Mechatronics and Power Engineering,Zhenjiang,China

Funder

National Natural Science Foundation of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9989533/9990034/09990277.pdf?arnumber=9990277

Reference21 articles.

1. Research on thermal protection by opposing jet and transpiration for high speed vehicle

2. Drag reduction Research in Supersonic Flow with Opposing Jet [J];rong;Acta Astronautica,2013

3. Numerical Study of the Effect of the Opposing Jet on Reduction of Aerodynamic Heating with Different Nose Configurations [C];tamada;26th International Congress of the Aeronautical Sciences Anchorage,2008

4. Reducing Aerodynamic Heating by the Opposing Jet in Supersonic and Hypersonic Flows

5. The effects of Maxwellian accommodation coefficient and free-stream Knudsen number on rarefied hypersonic cavity flows[J];xuhong;Aerospace Science and Technology,2020

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