Study on control of axisymmetric jet by half delta-wing shaped vortex generators (Part 1: Evaluation of statistics on the velocity field)-Reference-Cited by-同舟云学术

Study on control of axisymmetric jet by half delta-wing shaped vortex generators (Part 1: Evaluation of statistics on the velocity field)

Published:2015 Issue:828 Volume:81 Page:15-00306-15-00306
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

MIURA Kensuke¹,ITO Yasumasa¹,SAKAI Yasuhiko¹,IWANO Koji¹,NAGATA Koji²

Affiliation:

1. Department of Mechanical Science and Engineering, Nagoya University

2. Department of Aerospace Engineering, Nagoya University

Publisher

Japan Society of Mechanical Engineers

Link

https://www.jstage.jst.go.jp/article/transjsme/advpub/0/advpub_15-00306/_pdf

Reference17 articles.

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3. Carletti, M. J., Rogers, C. B. and Parekh, D. E., Parametric study of jet mixing enhancement by vortex generators, tabs and deflector plates, American Society of Mechanical Engineering, Fluids Engineering Division Conference, Vol.237 (1996), pp.303-312.

4. Enloe, C. L., McLaughlin, T. E., VanDyken, R. D., Kachner, K. D., Jumper, E. J., Corke, T. C. and Haddad, O., Mechanisms and responses of a single dielectric barrier plasma actuator: geometric effects, AIAA Journal, Vol.42 (2004), pp.595-604.

5. Fujita, S. and Osaka, H., Three-dimensional jets issuing from cruciform nozzles having four aspect ratios (1st report, mean flow properties), Transactions of the Japan Society of Mechanical Engineers, Series B, Vol.53, No.488 (1987), pp.1142-1149 (in Japanese).

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