Numerical Simulation of Jet Mixing in Supersonic Crossflow: Effect of Jet Exit Geometry-Reference-Cited by-同舟云学术

Numerical Simulation of Jet Mixing in Supersonic Crossflow: Effect of Jet Exit Geometry

Published:2022 Issue:4 Volume:65 Page:172-184
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

IWASA Toshihiro¹,TSUBOI Nobuyuki¹

Affiliation:

1. Department of Mechanical and Control Engineering, Kyushu Institute of Technology

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/65/4/65_T-21-25/_pdf

Reference34 articles.

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2. 2) Fujimoto, K. and Sakai, S.: Quantitative Crew Safety Analysis, JAXA Special Publication: Proceedings of Rocket and Spacecraft Modeling Laboratory Symposium 2018, Vol. JAXA-SP-18, 2018, pp. 47–60.

3. 3) Karagozian, A. R.: Transverse Jets and Their Control, Progr. Energy Combust. Sci., 36 (2010), pp. 531–553.

4. 4) Mahesh, K.: The Interaction of Jets with Crossflow, Annu. Rev. Fluid Mech., 45 (2013), pp. 379–407.

5. 5) Huang, W.: Transverse Jet in Supersonic Crossflows, Aerospace Science Technology, 50 (2016), pp. 183–195.

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