Hypersonics CFD Group



2011

  • Amjad Ali Pasha, K. Sinha, “Shock-unsteadiness model applied to hypersonic shock-wave/turbulent boundary-layer interactions” Journal of Propulsion and Power, 2010, Accepted
  • Amjad Ali Pasha, C. Vadivelan, K. Sinha, “Simulation of a practical scramjet inlet using shock-unsteadiness model” 28th International Symposium on Shock Waves, The University of Manchester, United Kingdom, 17-22 July 2011.
  • K. Sinha, Nilesh J. Rane and Vignesh Pawar, “Numerical Investigation of three Dimensional shock/boundary-layer interaction in a hypersonic inlet”, 28th International Symposium on shock waves, The University of Manchester, United Kingdom, 17-22 July 2011.
  • Reddy, D.S.K., and Sinha, K., Analysis of High-Enthalpy Air-chemistry and its Effect on Stagnation Point Heat Flux,Submitted to Journal of Thermophysics and Heat Transfer, June 2011.
  • Reddy, D.S.K., and Sinha, K., Effect of Chemical Reaction Rates on High-enthalpy Flow Prediction Around a Re-entry Capsule,Submitted to Journal of Thermophysics and Heat Transfer, June 2011.

2010

  • N. Rane, V. Pawar and K.. Sinha, “Effect of geometric variations on three-dimensional flow separation in a practical scramjet inlet”, 12th Annual AeSI CFD Symposium, Indian Institute of Science, Bangalore, India, 11-12 August, 2010.
  • D.S.K. Reddy and K. Sinha, Effect of Chemical Reaction Rates on Aero-heating Predictions of Re-entry Capsules, AIAA paper 2010-630, 2010.
  • A. Dey and K. Sinha, Simulation of Flow Separation and Reattachment on a Re-Entry Capsule Afterbody Frustum, AIAA paper 2010-1561, 2010.
  • A.A. Pasha and K. Sinha, Simulation of hypersonic shock/turbulent boundary-layer interactions using advanced turbulence models, The 8th Asian Computational Fluid Dynamics Conference, Hong Kong, China, 2010.
  • D.S.K Reddy and K. Sinha, Effect of chemical reaction rates on aero-heating predictions of re-entry flows, Vol. 25, No. 1, January-March 2011, Journal of Thermophysics and Heat Transfer.
  • N. Rane, V. Pawar and K. Sinha, “Effect of geometric variations on three-dimensional flow separation in a practical scramjet inlet”, 12th Annual AeSI CFD Symposium 2010, Indian Institute of Science, Bangalore, India, 2010..

2009

  • K. Sinha and V. Pawar, Shock/turbulence interaction: turbulence modeling and scramjet application, 11th Annual AeSI CFD Symposium 2009, Indian Institute of Science, Bangalore, India, 2009.
  • A.A. Pasha and K. Sinha, Simulation of three-dimensional shock/boundary-layer interaction in a single-fin configuration, 11th Annual AeSI CFD Symposium 2009, Indian Institute of Science, Bangalore, India, 2009.
  • D.S.K. Reddy and K. Sinha, Effect of Transport Coefficients on Aero-heating Predictions of Re-entry Capsules, Fourth Symposium on Applied Aerodynamics and Design of Aerospace Vehicles, Bangalore, India, Dec. 2009.
  • V. Pawar, N. Rane and K. Sinha, Three-dimensional Shock/Turbulent Boundary Layer Interaction in a Simulated Scramjet Inlet, Fourth Symposium on Applied Aerodynamics and Design of Aerospace Vehicles, Bangalore, India, Dec. 2009.
  • D.S.K. Reddy and K. Sinha, Hypersonic Turbulent Flow Simulation of Fire II Re-entry Vehicle Afterbody, Journal of Spacecrafts and Rockets, Vol.46, No.4, July-August 2009, pp. 745-757.
  • V. K. Veera and K. Sinha, Modeling the effect of upstream temperature fluctuations in shock/turbulence interaction, Physics of Fluids, Vol.21, No.2, 2009.

2008

  • K. Sinha and C.Vadivelan, Effect of Angle of Attack on Re-entry Capsule Afterbody Flowfield, AIAA Paper 2008-1282, 2008.
  • A.A. Pasha and K. Sinha, Shock-unsteadiness model applied to oblique shock wave/turbulent boundary-layer interaction, International Journal of Computational Fluid Dynamics, vol. 22, Issue 8, pp 569-582, September 2008.

2007

  • K. Sinha and S.K. Reddy, Hypersonic Turbulent Reacting Flow Simulation of Fire II Re-entry Vehicle, AIAA Paper 2007-805, 2007.
  • K. Sinha, Effect of Reynolds Number on Detached Eddy Simulation of Hypersonic Base Flows, AIAA Paper 2007-1457, 2007.
  • K. Sinha and G.V. Candler, Grid Sensitivity of Detached Eddy Simulation of a Mach 16 Re-Entry Configuration, AIAA Paper 2007-1115, 2007.
  • K. Sinha and C.Vadivelan, Reynolds-averaged Navier Stokes simulation of scramjet inlet flowfield, 7th Asian Computational Fluid Dynamics Conference, Bangalore, India, 2007.
  • A.A. Pasha and K. Sinha, Shock Unsteadiness Modification Applied to Oblique Shock Wave/Turbulent Boundary-Layer Interaction, 34th Fluid Mechanics Fluid Power Conference, Birla Institute of Technology and Science, Ranchi, India, Dec. 2007.
  • D.S.K. Reddy and K. Sinha, Analysis of Non-equilibrium Thermo-chemistry in Fire II Re-entry Flowfield, 34th Fluid Mechanics Fluid Power Conference, Birla Institute of Technology and Science, Ranchi, India, Dec. 2007 .

2006

  • K.S. Kedia and K. Sinha, Effect of Compressibility Corrections to Turbulence Models Applied to a Hypersonic Re-entry Configuration, 33r d National and 3rd International Conference on Fluid Mechanics and Fluid Power, Indian Institute of Technology Bombay, India, 2006 .
  • K. Sinha, Shock unsteadiness model applied to hypersonic shock-wave/turbulent boundary layer interactions, AIAA Papaer 2006-126, 2006.

2005

  • K. Sinha, RANS simulation of Fire II re-entry configuration, International Symposium on Shock Waves, Indian Institute of Science, Bangalore, India, 2005, pp 478-483, 2006.