Study of Separation Control of Vortex Generators on Transonic Wings-Reference-Cited by-同舟云学术

Study of Separation Control of Vortex Generators on Transonic Wings

Published:2011 Issue:1 Volume:6 Page:85-97
ISSN:1880-5558
Container-title:Journal of Fluid Science and Technology
language:en
Short-container-title:JFST

Author:

HUANG Jingbo¹,FU Song¹,XIAO Zhixiang¹,ZHANG Miao²

Affiliation:

1. School of Aerospace Engineering, Tsinghua University

2. Shanghai Aircraft Design and Research Institute of COMAC

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://www.jstage.jst.go.jp/article/jfst/6/1/6_1_85/_pdf

Reference22 articles.

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2. (2) Liu G., Liu W., Mou B. and Xiao Z.Y., CFD numerical simulation investigation of vortex generators, Acta Aerodynamica Sinica, Vol. 25, No. 2 2007, pp. 241-244.

3. (3) Ni Y. Q., Develoment of the vortex-generator and study on the effect of vortex-generator on boundary layer, Acta Aerodynamica Sinica, Vol. 13 1995, pp. 110-116.

4. (4) Lin J. C., Review of research on low-profile vortex generators to control boundary-layer separation, Progress in Aerospace Sciences, Vol. 38 2002, pp. 389-420.

5. (5) Yao C. S., Lin J. C. and Allan B. G., Flow-field measurement of device-induced embedded streamwise vortex on a flat plate, AIAA, 2002-3162.

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