Flow Field and Combustion Field Control Using Pylons Installed Upstream of a Cavity in Supersonic Flow-Reference-Cited by-同舟云学术

Flow Field and Combustion Field Control Using Pylons Installed Upstream of a Cavity in Supersonic Flow

Published:2020 Issue:2 Volume:63 Page:50-61
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:

HIZAWA Tomohiro¹²,YAMAGUCHI Tatsuya¹²,MURATA Ko¹²,YUGAMI Yasuto¹²,HASEGAWA Mariko¹²,KUDO Taku²,HAYAKAWA Akihiro²,KOBAYASHI Hideaki²

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Tohoku University

2. Institute of Fluid Science, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/63/2/63_T-19-14/_pdf

Reference14 articles.

1. 1) Daines, R. and Segal, C.: Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications, J. Propul. Power, 14 (1998), pp. 605–612.

2. 2) Yamaguchi, T., Ichikawa, T., Hizawa, T., Kudo, T., Hayakawa, A., and Kobayashi, H.: Effects of Boundary Layer Thickness on Flameholding of Cavityholder with a Bottom Single Hole Injector, 55th Symposium (Japanese) on Combustion, 2017, pp. 388–389 (in Japanese).

3. 3) Aguilera, C., Pang, B., Ghosh, A., Winkelmann, A., Gupta, A. K., and Yu, K. H.: Supersonic Mixing Enhancement and Optimization Using Fin-Guided Fuel Injection, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, No. 1526, 2010.

4. 4) Aguilera, C. and Yu, K. H.: Supersonic Mixing Enhancement Using Fin-Guided Fuel Injection, J. Propul. Power, 31 (2015), pp. 1532–1543.

5. 5) Freeborn, A. B., King, P. I., and Gruber, M. R.: Characterization of Pylon Effects on a Scramjet Cavity Flameholder Flowfield, AIAA Paper 08-86, 2008.

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