def compute(self, inputs, outputs): outputs['radius'] = radii(inputs['mesh'], self.options['surface']['t_over_c'])
def compute(self, inputs, outputs): outputs['radius'] = radii(inputs['mesh'], inputs['t_over_c'])
def compute(self, inputs, outputs): mesh = inputs['mesh'] t_over_c = inputs['t_over_c'] max_radius = radii(mesh, t_over_c) outputs['spar_within_wing'] = inputs['radius'] - max_radius
def compute(self, inputs, outputs): mesh = inputs['mesh'] max_radius = radii(mesh, self.surface['t_over_c']) outputs['spar_within_wing'] = inputs['radius'] - max_radius