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Rohan Morajkar
Rohan Morajkar
Graduate student research assistant, Aerospace Engineering, University of Michigan
Verified email at umich.edu
Title
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Cited by
Year
Relationship between intermittent separation and vortex structure in a three-dimensional shock/boundary-layer interaction
RR Morajkar, RL Klomparens, WE Eagle, JF Driscoll, M Gamba, JA Benek
AIAA Journal 54 (6), 1862-1880, 2016
312016
Turbulence characteristics of supersonic corner flows in a low aspect ratio rectangular channel
RR Morajkar, M Gamba
54th AIAA Aerospace Sciences Meeting, 1590, 2016
132016
Experimental study of supersonic turbulent corner flow evolution in a low aspect ratio rectangular channel
RR Morajkar, JF Driscoll, M Gamba
53rd AIAA Aerospace Sciences Meeting, 0542, 2015
112015
Flow Separation Associated with 3-D Shock-Boundary Layer Interaction (SBLI)
RR Morajkar, RL Klomparens, WE Eagle, JF Driscoll, M Gamba
52nd Aerospace Sciences Meeting, 1138, 2014
72014
Role of Secondary Flows on Flow Separation Induced by Shock/Boundary-Layer Interaction in Supersonic Inlets
R Morajkar
62017
Swept shock corner flow interacions
RR Morajkar, M Gamba
54th AIAA Aerospace Sciences Meeting, 1165, 2016
52016
Energy vapor exchanger with an inlet vortex generator
R Morajkar
US Patent App. 17/684,898, 2023
2023
Relationship Between Intermittent Separation and Vortex Structure in a 3D Shock-Boundary Layer Interaction
RR Morajkar, RL Klomparens, WE Eagle, JF Driscoll, M Gamba, JA Benek
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