CompAero/RayleighFlowRelations.py
def calc_mach_from_Rho_RhoStar(rho_rhoSt: float, gamma: float) -> float:
        """Calculates the mach number based of the ratio of density to sonic density Rho/Rho*

        Args:
            rho_rhoSt (float): Ratio of density to sonic density Rho/Rho*
            gamma (float): ratio of specific heats

        Returns:
            float: mach number
        """
        return brenth(RayleighFlowRelations.calc_Rho_RhoStar, 1e-9, 40, args=(gamma, rho_rhoSt,))
Calculates the mach number based of the ratio of density to sonic density Rho/Rho*

        Args:
            rho_rhoSt (float): Ratio of density to sonic density Rho/Rho*
            gamma (float): ratio of specific heats

        Returns:
            float: mach number
        
Calculates the mach number based of the ratio of density to sonic density Rho/Rho
Calculates the mach number based of the ratio of density to sonic density Rho / Rho
def calc_mach_from_Rho_RhoStar(rho_rhoSt: float, gamma: float) -> float:
        return brenth(RayleighFlowRelations.calc_Rho_RhoStar, 1e-9, 40, args=(gamma, rho_rhoSt,))
def calc_mach_from_Rho_RhoStar ( rho_rhoSt : float , gamma : float ) -> float : return brenth ( RayleighFlowRelations . calc_Rho_RhoStar , 1e-9 , 40 , args = ( gamma , rho_rhoSt , ) )
Calculates the mach number based of the ratio of density to sonic density Rho/Rho
Calculates the mach number based of the ratio of density to sonic density Rho / Rho
"""Calculates the mach number based of the ratio of density to sonic density Rho/Rho*

        Args:
            rho_rhoSt (float): Ratio of density to sonic density Rho/Rho*
            gamma (float): ratio of specific heats

        Returns:
            float: mach number
        """
None
float
rho_rhoSt
float
Ratio of density to sonic density Rho/Rho
Ratio of density to sonic density Rho / Rho
gamma
float
ratio of specific heats
ratio of specific heats