Effects of dual jets distance on mixing characteristics and flow path within a cavity in supersonic crossflow-Reference-Cited by-同舟云学术

Effects of dual jets distance on mixing characteristics and flow path within a cavity in supersonic crossflow

Published:2014-12 Issue: Volume:50 Page:254-262
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Ukai Takahiro,Zare-Behtash Hossein,Lo Kin Hing,Kontis Konstantinos,Obayashi Shigeru

Publisher

Elsevier BV

Subject

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

Reference32 articles.

1. Effects of injector yaw on mixing characteristics of aerodynamic ramp injectors;Cox-Stouffer;AIAA Paper,1999

2. Drummond, J.P., Bouchez, M., McClinton, C.R., 2006. Overview of NATO background on scramjet technology. NASA Techdoc 20060020216.

3. Experimental investigation of transverse injection flowfield at Mach 5 and the influence of impinging shock wave;Erdem;AIAA Paper,2012

4. Erdem, E., Saravanan, S., Kontis, K., 2012. Air, carbon dioxide and helium transverse sonic jets in Mach 5 cross flow. In: 9th International ERCOFTAC Symposium on Engineering Turbulence Modelling and Measurements.

5. Influence of shock wave propagation on dielectric barrier discharge plasma actuator performance;Erfani;J. Phys. D Appl. Phys.,2012

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