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
def compute(self, inputs, outputs):
outputs['radius'] = radii(inputs['mesh'], inputs['t_over_c'])
