55th AIAA Aerospace Sciences Meeting 2017
DOI: 10.2514/6.2017-0490
|View full text |Cite
|
Sign up to set email alerts
|

Numerical Investigation on the Oblique Shock and High-speed Vortex Rings Interaction

Abstract: A wedge-shaped micro vortex generator is placed on a flat plate over which a turbulent boundary layer at Mach number 2.5 is developed. The interaction between an oblique shock wave and high-speed vortex rings in the MVG controlled ramp flow is investigated by using a high order implicit large eddy simulation with the fifth order bandwidth optimized WENO scheme. The vortical structures are visualized using the Omega identification method proposed by UTA researchers. By tracking several typical vortex rings befo… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
0
0

Publication Types

Select...

Relationship

0
0

Authors

Journals

citations
Cited by 0 publications
references
References 27 publications
0
0
0
Order By: Relevance

No citations

Set email alert for when this publication receives citations?