English
हिन्दी
IMPRANS
IMPRANS (RANS Solver for Unsteady Compressible Flows)
Implicit Finite volume nodal point scheme using structured boundary fitted grid. Dual time stepping and Baldwin Lomax turbulence model for 3-D unsteady viscous compressible flows.
Applications to Steady flow simulations, Unsteady flow simulations and Aeroelastic Analysis
TURBULENT FLOW PAST A PITCHING AEROFOIL
FLOW AROUND A LIFTING HELICOPTER ROTOR BLADE IN FORWARD FLIGHT
Pressure fields on upper and lower surface of the rotor blade
