Simulation of large scales and aeroacoustics of perfectly expanded supersonic jets
COMPUTATIONAL SIMULATION OF COMPRESSIBLE FLOWS IN THE RAE 2822 AERODYNAMIC PROFILE
Development of Reduced Order Modeling Approaches for Nonlinear Aeroelastic Analyses
Investigation of shock-boundary layer interactions in supersonic axial turbines
Numerical analysis of boundary layer transition caused by asymmetric cavities.
Development of Reduced Order Modeling Approaches for Nonlinear Aeroelastic Analyses
Numerical methods in the solution of aeroelastic equations of airfoil in transonic...