• CFD Prediction of Re-entry Heating

Fire II re-entry capsule at 35 km altitude

CFD simulation with non-equilibrium thermo-chemistry

3D unsteady flow simulation at Mach 16

• HSTDV forebody simulation at Mach 6.5

HSTDV forebody simulation at Mach 6.5
HSTDV forebody with bi-curvature nose

3D shock structure around forebody

• Three-dimensional flow analysis of ISRO intake

Scramjet module attached on rocket

Intake Geometry

Complex shock structure on side wall 

Flow separation inside intake duct