![]() Indigenous CFD codes were developed and routinely used to generate aerodynamic design data in complete M-α-δ-φ flight envelope. His most noteworthy contribution in VSSC was aerodynamic parameters prediction of heat shield separation test in ground.Īt DRDL (Nov’01-Nov’19) as Technology Director (Computational Dynamics), Group Director (Design) and Associate Director (Technology), he provided leadership to develop core competence in missile design for both tactical and strategic applications. The interaction of different propulsive jets from strap-on and main rocket motors and with free stream supersonic flows at different altitudes were analysed analytically and numerically to provide design data of base pressures and convective heat fluxes. His Ph.D dissertation is on Direct Numerical Simulation (DNS) studies in high-speed confined mixing layer in chemically reacting environment which have brought out many important issues of high-speed mixing and combustion.Īt VSSC (Sep’86-Nov’01), he contributed significantly in launch vehicle base flow analysis and provided vital inputs for thermal protection system design. He did his M.Sc in Applied Mathematics from Jadavpur University, M.Tech in Computational Mechanics from IIT, Kharagpur and Ph.D in Aerospace Engineering from IISc, Bengaluru. Debasis Chakraborty had experience in working for 35 years on variety of complex physical problems at Vikram Sarabhai Space Centre (VSSC), Thiruvananthapuram and Defense Research and Development Laboratory (DRDL), Hyderabad and Indian Institute of Technology (IIT), Bombay. Computer Aided Structural Engineering Program.Electronics and Communication Engineering.
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