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ivc = get_indep_var_comp(input_list) |
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if low_speed_aero: |
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ivc.add_output("data:aerodynamics:aircraft:low_speed:oswald_coefficient", mach) |
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else: |
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ivc.add_output("data:aerodynamics:aircraft:cruise:oswald_coefficient", mach) |
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problem = run_system(InducedDragCoefficient(low_speed_aero=low_speed_aero), ivc) |
Why oswald_coefficient = mach in this test?
