Clarification required for total pressure increase
I am studying Stationary turbine blade aerodynamics. Flow is compressible.
solver - density based-implicit material-ideal gas
My total pressure is increasing near the leading edge of the blade. (slightly higher then inlet Total pressure).
There is no energy addition in the domain, but total pressure is increasing slightly.
Please give clarification on this.
|All times are GMT -4. The time now is 13:50.|