Current Research
Our current research is:
- Large Eddy Simulation (LES) of supersonic flow over expansion compression corner: In this project, the LES of supersonic flow over expansion compression corner will be performed at different expansion-compression angles. The results will be compared with experimental data. The main purpose of this work is to examine the accuracy of the new recycling-rescaling method (Ht&p) in the prediction of surface pressure and pressure profiles at different locations at high supersonic speeds.
Previous Research
Our previous research topics are:
- Large Eddy Simulation of hypersonic flow over cold wall flat plate
- Prediction of aerothermodynamic loading of Edney III type shock-shock interaction over a hemisphere at hypersonic speeds
- Prediction of aerothermodynamic loading of shock wave laminar boundary layer interaction
over hollow cylinder flare and double cone at hypersonic flows
- Energy discharge for drag reduction
- Energy discharge for flight control