Study on the drag and heat reduction performance of porous opposing jet in hypersonic flow-Reference-Cited by-同舟云学术

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Study on the drag and heat reduction performance of porous opposing jet in hypersonic flow

Published:2019-08 Issue: Volume:139 Page:351-361
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Fan Wei-jie,Li Shi-bin,Zhou Jin,Huang Wei,Ou Min,Zhang Rui-rui

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference42 articles.

1. Effect of spike on steady and unsteady flow over a blunt body at supersonic speed;Sahoo;Acta Astronaut.,2016

2. S. Aso, T. Kurotaki, Y. Miyamoto, Y. Isomura, R. Kurosaki, and M. Katayama, Experimental and Computational Study on Reduction of Aerodynamic Heating Load by Film Cooling in hypersonic flows; 1997: AIAA 97-0770.

3. S. Aso, K. Hayashi, M. Mizoguchi, A study on aerodynamic heating reduction due to opposing jet in hypersonic flow; 2002, AIAA 2002-0646.

4. Numerical experiment on the flow field properties of a blunted body with a counterflowing jet in supersonic flows;Huang;Acta Astronaut.,2018

5. The flow of a jet from a body opposing a supersonic free stream;Finley;J. Fluid Mech.,1966

Cited by 16 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Angle-of-attack characteristics of opposing jet for improving drag and heat reduction;Physics of Fluids;2024-07-01

2. Numerical Investigation on the Thermal Protection Characteristics of a New Active Jet Design Parameter for Hypersonic Flight Vehicle;International Journal of Aerospace Engineering;2023-03-24

3. Numerical study of reverse jet for mitigating shock/shock interaction heating;Aerospace Science and Technology;2022-12

4. Fluid-thermo-structural response of actively cooled scramjet combustor in hypersonic accelerating-cruise flight;International Journal of Heat and Mass Transfer;2022-09

5. Investigation on the Opposing Jet in the Hypersonic Rarefied Flow over a Vehicle Based on the DSMC Method;Actuators;2022-06-15

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