CompAero/ObliqueShockRelations.py
def calc_mach_normal_behind_shock_from_mach_behind_shock(
        mach2: float, beta: float, theta: float
    ) -> float:
        """ Calculates the normal component of the mach number behind the oblique shock 

        Args:
            mach2 (float): Mach number of flow behind the oblique shock
            beta (float): Oblique shock angle (radians)
            theta (float): Flow deflections (Wedge) angle (radians)

        Returns:
            float: Normal component of mach numnber of the flow behind the shock wave
        """
        return mach2 * sin(beta - theta)
 Calculates the normal component of the mach number behind the oblique shock 

        Args:
            mach2 (float): Mach number of flow behind the oblique shock
            beta (float): Oblique shock angle (radians)
            theta (float): Flow deflections (Wedge) angle (radians)

        Returns:
            float: Normal component of mach numnber of the flow behind the shock wave
        
Calculates the normal component of the mach number behind the oblique shock
Calculates the normal component of the mach number behind the oblique shock
def calc_mach_normal_behind_shock_from_mach_behind_shock(
        mach2: float, beta: float, theta: float
    ) -> float:
        return mach2 * sin(beta - theta)
def calc_mach_normal_behind_shock_from_mach_behind_shock ( mach2 : float , beta : float , theta : float ) -> float : return mach2 * sin ( beta - theta )
Calculates the normal component of the mach number behind the oblique shock
Calculates the normal component of the mach number behind the oblique shock
""" Calculates the normal component of the mach number behind the oblique shock 

        Args:
            mach2 (float): Mach number of flow behind the oblique shock
            beta (float): Oblique shock angle (radians)
            theta (float): Flow deflections (Wedge) angle (radians)

        Returns:
            float: Normal component of mach numnber of the flow behind the shock wave
        """
Normal component of mach numnber of the flow behind the shock wave
Normal component of mach numnber of the flow behind the shock wave
float
mach2
float
Mach number of flow behind the oblique shock
Mach number of flow behind the oblique shock
beta
float
Oblique shock angle (radians)
Oblique shock angle ( radians )
theta
float
Flow deflections (Wedge) angle (radians)
Flow deflections ( Wedge ) angle ( radians )