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Shock-wave/boundary layer interaction control using spark-jet and micro-vortex generator

Fang, Jian; Yang, Guang; Yao, Yufeng; Liu, Chaoqun; Lu, Lipeng

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Authors

Jian Fang

Guang Yang

Yufeng Yao Yufeng.Yao@uwe.ac.uk
Professor in Aerospace Engineering

Chaoqun Liu

Lipeng Lu



Abstract

We present Large-Eddy Simulation of two control devices: active control by SparkJet and passive control by MVG. It is found that both methods can greatly alleviate the separation. Flowfield analysis shows that the streamwise counter-rotating vortex generated by the two devices might be the common control mechanism.

Citation

Fang, J., Yang, G., Yao, Y., Liu, C., & Lu, L. (2016, September). Shock-wave/boundary layer interaction control using spark-jet and micro-vortex generator. Poster presented at UKTC Annual Workshop, Cambridge, UK

Presentation Conference Type Poster
Conference Name UKTC Annual Workshop
Conference Location Cambridge, UK
Start Date Sep 1, 2016
End Date Sep 2, 2016
Acceptance Date Sep 1, 2016
Publication Date Jan 1, 2016
Publicly Available Date Jun 7, 2019
Peer Reviewed Peer Reviewed
Keywords shock-wave, spark-jet, micro-vortex
Public URL https://uwe-repository.worktribe.com/output/918711
Additional Information Title of Conference or Conference Proceedings : UKTC Annual workshop Sept 2016

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