Ph.D., Aerospace Engineering, University of Texas at Arlington, 1988 - Extended the numerical scheme, Direct Formal Integration, to solve compressible boundary layer flows
M.S., Aerospace Engineering, University of Texas at Arlington, 1984 - Extended the numerical scheme, Direct Formal Integration, to solve incompressible boundary layer flows
B.Tech., Aeronautical Engineering, IIT Madras, 1982 - Developed Euler equation solver on the surface of sphere to compute flow past a cone at an angle of attack in supersonic flow using shock fitting
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