CompAero/FannoFlowRelations.py
def calc_mach_from_U_USt(u_uSt: float, gamma: float) -> float:
        """Calculates the mach number based of the ratio of velocity to sonic velocity U/U*

        Args:
            u_uSt (float): Ratio of velocity to sonic velocity U/U*
            gamma (float): ratio of specific heats

        Returns:
            float: mach number
        """
        return brenth(FannoFlowRelations.calc_U_UStar, 1e-9, 40, args=(gamma, u_uSt))
Calculates the mach number based of the ratio of velocity to sonic velocity U/U*

        Args:
            u_uSt (float): Ratio of velocity to sonic velocity U/U*
            gamma (float): ratio of specific heats

        Returns:
            float: mach number
        
Calculates the mach number based of the ratio of velocity to sonic velocity U/U
Calculates the mach number based of the ratio of velocity to sonic velocity U / U
def calc_mach_from_U_USt(u_uSt: float, gamma: float) -> float:
        return brenth(FannoFlowRelations.calc_U_UStar, 1e-9, 40, args=(gamma, u_uSt))
def calc_mach_from_U_USt ( u_uSt : float , gamma : float ) -> float : return brenth ( FannoFlowRelations . calc_U_UStar , 1e-9 , 40 , args = ( gamma , u_uSt ) )
Calculates the mach number based of the ratio of velocity to sonic velocity U/U
Calculates the mach number based of the ratio of velocity to sonic velocity U / U
"""Calculates the mach number based of the ratio of velocity to sonic velocity U/U*

        Args:
            u_uSt (float): Ratio of velocity to sonic velocity U/U*
            gamma (float): ratio of specific heats

        Returns:
            float: mach number
        """
None
float
u_uSt
float
Ratio of velocity to sonic velocity U/U
Ratio of velocity to sonic velocity U / U
gamma
float
ratio of specific heats
ratio of specific heats