Breakdown of Counter-Rotating Supersonic Streamwise Vortices Generated by Swept Ramp Injector-Reference-Cited by-同舟云学术

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Breakdown of Counter-Rotating Supersonic Streamwise Vortices Generated by Swept Ramp Injector

Published:2018 Issue:2 Volume:16 Page:172-176
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

SAKAUE Shoji¹,SHICHIRI Shingo¹,TSUKAZAKI Yamato¹,HASHIMOTO Kazuma¹,ARAI Takakage¹

Affiliation:

1. Department of Aerospace Engineering, Osaka Prefecture University

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/16/2/16_172/_pdf

Reference18 articles.

1. 1) Scuderi, L. F., Orton, G. F., and Hunt, J. L.: Mach 10 Cruise/Space Access Vehicle Definition, AIAA Paper 1998-1584, 1998.

2. 2) Yamauchi, Y., Kodama, Y., Sakaue S., and Arai, T.: Effect of Mach Number on Supersonic Mixing by ”Hyper-Mixer Injector”, AIAA Paper 2012-5816, 2012.

3. 3) Arai, T., Yamauchi, Y., and Sakaue, S.: Effect of Incoming Boundary Layer on Supersonic Mixing Layer Generated by Wall-Mounted Ramp Injector, AIAA Paper 2014-3216, 2014.

4. 4) Tsukazaki, Y., Sakaue, S., and Arai, T.: Mach Number Effect on Breakdown of Streamwise Vortices in Supersonic Flow, AJCPP 2016, March. 2016.

5. 5) Barber, M. J., Schetz, J. A., and Roe, L. A.: Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice into Supersonic Flow, J. Propulsion and Power, 13(1997), pp. 257–263.

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