Thermal engineering
The development of thermal protection system against the aerodynamic heating during atmospheric-entry is crucial for a space transportation system including planetary exploration vehicle, space plane and re-entry capsule.
• Ablation Thermal Protection Systems during atmospheric entry maneuvers; suitability of ablation systems to thermal protection depends on complex physical and chemical processes.
• Prediction and evaluation of heat-flux during entry of a spacecraft
Computational Fluid Dynamics (CFD)
Computational fluid dynamics for aerothermodynamics and plasmas
Atmospheric entry Problem Analysis
Reaction Control System (RCS) Analysis for Missile and Re-entry Capsule
Modelling and Numerical Simulation of Multi-Physical Problems
