contra rotating vortex generator configuration.
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Hydrogen mixing augmentation mechanism induced by the vortex generator and oblique shock wave in a scramjet engine - ScienceDirect
Fluids, Free Full-Text
lift and drag coefficients for the airfoil NACA 63-430
Vortex Generator (Chapter 3) - Flow Control Techniques and Applications
Experimental study of counter-rotating vortex pair trajectories induced by a round jet in cross-flow at low velocity ratios
Hernan CERÓN-M, Professor (Assistant), Postdoc, University of São Paulo, São Paulo, USP, Departamento de Engenharia Aeronáutica (SAA) (São Carlos)
pressure coefficient distribution (cp) for the airfoil NACA 63-215 at
pressure coefficient distribution (cp) for the airfoil NACA 63-215 at
a) Counter-rotating and (b) co-rotating vortices.
Micro-vortex generators for shock wave/boundary layer interactions - ScienceDirect
Vortex generator geometry. Download Scientific Diagram
Interactions of a counter-rotating vortex pair at multiple offsets
pressure coefficient distribution (cp) for the airfoil NACA 63-215 at
