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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

Aircraft Aerodynamics

Thermal engineering

Modelling and Numerical Simulation of Multi-Physical Problems