A superior 1-D analytical model in MATLAB for gaseous film cooling applicable to rocket nozzles has been developed, which takes into account
- the effect of mixing,
- coolant injection on the velocity profile,
- radiation
- and freestream turbulence.
This repository contains MATLAB script tuned for gaseous cooling for 1D flat plate and in progress for extending for a specific genric rocket nozzle.
Reuslts:
Comparision of 1D analytical model to experimnet found in literature.
Validation work: Fluent simulation to validate the current 1d analytical model
