Development of an Efficient Numerical Scheme for the Computation of Turbulent Boundary Layer Flows Over Two-dimensional and Axisymmetric Bodies
Investigation of Aerodynamic Characteristics of Wings Having Vortex Flow Using Different Numerical Codes
Development of Dynamic Pressure Calibration Techniques Under Thermal Environment for Use in Powered Lift Airfoil Research
Computations in Turbulent Flows and Off-design Performance Predictions for Airframe-integrated SCRAMjets
Synthesis of a Control Model for a Liquid Nitrogen Cooled, Closed Circuit, Cryogenic Nitrogen Wind Tunnel and Its Validation