clcd¶
-
class
clcd.
CLCD
(**kwargs)[source]¶ Bases:
openmdao.components.meta_model_structured_comp.MetaModelStructuredComp
Computes aerodynamic lift and drag coefficients from aerodynamics data tables.
The CLCD component requires the following inputs:
inputs['alpha']
: aircraft angle of attack [deg]inputs['theta_flaps']
: aircraft flap deflection angle [deg]inputs['theta_slats']
: aircraft slat deflection angle [deg]
The CLCD component computes the following outputs:
outputs['c_l']
: aircraft lift coefficient [-]outputs['c_l_max']
: maximum aircraft lift coefficient [-]outputs['c_d']
: aircraft drag coefficient [-]