The Indian Space Research Organisation (ISRO) has developed Computational Fluid Dynamics (CFD) software named Parallel RANS Solver for Aerospace Vehicle Aero-thermo-dynamic Analysis (PraVaHa).
This software was developed in ISRO’s Vikram Sarabhai Space Centre (VSSC). It can simulate external and internal flows on launch vehicles, winged and non winged re-entry vehicles.
According to ISRO, initial aerodynamic design studies for launch vehicles demand evaluation of a large number of configurations.
Any aerospace vehicle while moving through the Earth’s atmosphere during launch or re-entry is subjected to severe aerodynamic and aerothermal loads in terms of external pressure and heat flux.
Understanding the airflow around aircraft, rocket bodies, or Crew Module (CM) during earth re-entry is essential to design the shape, structure, and Thermal Protection System (TPS) required for these bodies.