Module MAPLEAF.Rocket.CythonFinFunctions

Cython functions to speed up the FinSet aerodynamic model

Functions

def getFinSliceAngleOfAttack(...)

Finds the AOA of the present a fin slice. Limits AOA to a magnitude of stallAngle

def getFinSliceForce_Supersonic(...)

Computes normal force produced by a supersonic fin surface slice, excluding dynamic pressure. Supersonic correlations, Eq. 3.41-3.44 (Niskanen) Using third-order Busemann expansion, was also used by Barrowman. Mach Cone correction applied in parent function

def getSubsonicFinNormalForce(...)

def getSupersonicFinNormalForce(...)