Experimental investigation on flow characteristics of a transverse jet with an upstream vortex generator-Reference-Cited by-同舟云学术

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Experimental investigation on flow characteristics of a transverse jet with an upstream vortex generator

Published:2020-08 Issue:8 Volume:21 Page:636-651
ISSN:1673-565X
Container-title:Journal of Zhejiang University-SCIENCE A
language:en
Short-container-title:J. Zhejiang Univ. Sci. A

Author:

Zhao Yan-hui^ORCID,Liang Jian-han,Zhang Shun-ping,Ren Hong-yu,Zhao Yu-xin,Yang Shun-hua

Funder

National Natural Science Foundation of China

the Fenglei Youth Innovation Fund of China Aerodynamics Research and Development Center

Publisher

Zhejiang University Press

Subject

General Engineering

Link

https://link.springer.com/content/pdf/10.1631/jzus.A1900392.pdf

Reference37 articles.

1. Anderson B, Tinapple J, Surber L, 2006. Optimal control of shock wave turbulent boundary layer interactions using micro-array actuation. Proceedings of the 3rd AIAA Flow Control Conference. https://doi.org/10.2514/6.2006-3197

2. Babinsky H, Li Y, Ford CWP, 2009. Microramp control of supersonic oblique shock-wave/boundary-layer interactions. AIAA Journal, 47(3):668–675. https://doi.org/10.2514/1.38022

3. Bogdanoff DW, 1994. Advanced injection and mixing techniques for scramjet combustors. Journal of Propulsion and Power, 10(2):183–190. https://doi.org/10.2514/3.23728

4. Chen F, Liu H, Rong Z, 2012. Development and application of nanoparticle tracers for PIV in supersonic and hypersonic flows. Proceedings of the 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.

5. Chen F, Liu H, Yang ZF, et al., 2017. Tracking characteristics of tracer particles for PIV measurements in supersonic flows. Chinese Journal of Aeronautics, 30(2):577–585. https://doi.org/10.1016/j.cja.2016.12.033

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