Expand description
Collection of functions for isentropic compressible flow. TODO: finish documentation
Functionsยง
- mach_
from_ a_ ac - Mach number for a given critical area ratio.
- mach_
from_ f_ mcpt0 - mach_
from_ mach_ angle - Mach number for a given mach angle in radians.
- mach_
from_ mcpt0_ ap - mach_
from_ mcpt0_ ap0 - mach_
from_ normal_ mach2 - mach_
from_ normal_ p02_ p01 - mach_
from_ p0_ p - mach_
from_ p_ p0 - Mach number for a given total pressure ratio.
- mach_
from_ pm_ angle - Mach number for a given Prandtl-Meyer angle in radians.
- mach_
from_ rho0_ rho - mach_
from_ rho_ rho0 - Mach number for a given stagnation density ratio.
- mach_
from_ t0_ t - Mach number for a given total temperature ratio.
- mach_
from_ t_ t0 - Mach number for a given total temperature ratio.
- mach_
from_ v_ cpt0