python API
BladeRow
Coolant
LossType
PassageType
PowerType
RowType
Inlet
A_As()
FindMachP0P()
IsenP()
IsenT()
Massflow()
solve_for_mach()
LossInterp
Outlet
Passage
radeq()
adjust_streamlines()
TurbineSpool
T0_coolant_weighted_average()
compute_quantities()
compute_reynolds()
inlet_calc()
rotor_calc()
stator_calc()
Solves the radial equilibrium equation for axial machines and returns the convergence.
Note
This function will give you T0, P0, Vm as a function of the radius.
row (BladeRow) – Current row
upstream (BladeRow) – Previous row
downstream (BladeRow) – Next row
current row with T0, P0, and Vm calculated