Print Email Facebook Twitter Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow Title Experimental Characterization of a Micro-ramp Wake and its Flow Mixing Properties in Supersonic Flow Author Srivastava, A. (TU Delft Aerospace Engineering) Contributor van Oudheusden, Bas (mentor) Schrijer, Ferdinand (mentor) Elsinga, Gerrit (mentor) Giepman, Rogier (mentor) Degree granting institution Delft University of Technology Programme Aerospace Engineering | Aerodynamics and Wind Energy Date 2014-08-19 Abstract Micro-ramps are currently being investigated as a means of reducing negative effects of shock wave-turbulent boundary layer interactions. A micro-ramp enhances the mixing of the ow by introducing vortices in the ow, thus energizing the boundary layer to overcome the adverse pressure gradient due to an impinging shock. The effect of changing micro-ramp height, Mach number and Reynolds number on the mean ow downstream of a micro-ramp's center-line has been studied extensively. To reference this document use: http://resolver.tudelft.nl/uuid:084f2da6-d554-4b51-b605-e10a0f1d1785 Part of collection Student theses Document type master thesis Rights © 2014 A. Srivastava Files PDF Srivastava_A..pdf 30.75 MB Close viewer /islandora/object/uuid:084f2da6-d554-4b51-b605-e10a0f1d1785/datastream/OBJ/view