Control of Incident Shock-Induced Separation Using Vane-Type Vortex-Generating Devices | Zendy

Shashi B. Verma | Zendy; C. Manisankar | Zendy

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Control of Incident Shock-Induced Separation Using Vane-Type Vortex-Generating Devices

Author(s) -

Shashi B. Verma,

C. Manisankar

Publication year - 2018

Publication title -

aiaa journal

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.828

H-Index - 158

eISSN - 1081-0102

pISSN - 0001-1452

DOI - 10.2514/1.j056460

Subject(s) - mach number , separation (statistics) , flow separation , shock (circulatory) , vortex generator , mechanics , vortex , reduction (mathematics) , materials science , boundary layer , control theory (sociology) , flow control (data) , physics , mathematics , geometry , control (management) , engineering , computer science , medicine , telecommunications , statistics , artificial intelligence

An experimental investigation was conducted to control an incident shock-induced boundary-layer separation associated with a 14 deg shock generator in a Mach 2.05 flow. Two vane-type configurations...

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