aerosandbox.geometry.airfoil.default_airfoil_aerodynamics¶

Functions¶

`default_CL_function`(alpha, Re[, mach, deflection])	Lift coefficient.
`default_CD_function`(alpha, Re[, mach, deflection])	Drag coefficient.
`default_CM_function`(alpha, Re[, mach, deflection])	Pitching moment coefficient, as measured about quarter-chord.

Module Contents¶

aerosandbox.geometry.airfoil.default_airfoil_aerodynamics.default_CL_function(alpha, Re, mach=0, deflection=0)[source]¶: Lift coefficient.

aerosandbox.geometry.airfoil.default_airfoil_aerodynamics.default_CD_function(alpha, Re, mach=0, deflection=0)[source]¶: Drag coefficient.

aerosandbox.geometry.airfoil.default_airfoil_aerodynamics.default_CM_function(alpha, Re, mach=0, deflection=0)[source]¶: Pitching moment coefficient, as measured about quarter-chord.