Department of  Aerospace  Engineering
 Indian Institute of Technology, Bombay
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Shock / Turbulent Boundary Layer Interaction in Scramjet Inlets

  • Modeling shock unsteadiness in shock/turbulence interaction
  • Reynolds-averaged Navier Stokes simulation of scramjet inlet flowfield
  • Shock-Unsteadiness Model Applied to Oblique Shock Wave/ Turbulent Boundary-Layer Interaction
  • Modeling the effect of upstream temperature fluctuations on shock/homogeneous turbulence interaction
  • Simulation of three-dimensional shock/boundary-layer interaction in a single-fin configuration
  • Three-dimensional shock/turbulent boundary layer interaction in a simulated scramjet inlet
  • Simulation of Hypersonic Shock/Turbulent Boundary-Layer Interactions using Advanced Turbulence Models
  • Effect of Geometric Variations on Three-Dimensional Flow Separation in a Practical Scramjet Inlet

Simulation of Re-entry Capsule Afterbody Flowfield.

  • Hypersonic Turbulent Flow Simulation of FIRE II Reentry Vehicle Afterbody
  • Detached eddy simulation of a Mach 16 Re-entry Configuration
  • Effect of Angle of Attack on Re-entry Capsule Afterbody Flowfield
  • Simulation of Flow Separation and Reattachment on a Re-entry Capsule Afterbody Frustum
  • Effect of Transport Coefficients on Aero-thermal Predictions of Reentry Flows
  • Effect of Chemical Reaction Rates on Aero-Heating Predictions of Re-entry Flows
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