@@ -0,0 +1,406 @@
+from collections import defaultdict%0Aimport pytest%0Afrom wingstructure.aero.multhop import AirfoilData%0Afrom wingstructure.aero.aero_moment import mean_momentcoefficient%0A%0Afrom .test_data_wing import d38wing%0A%0Adef test_meanmomentcoefficient(d38wing):%0A%0A    afdat = AirfoilData(c_m0=0.03)%0A%0A    airfoil_db = defaultdict(lambda: afdat)%0A%0A    C_m0 = mean_momentcoefficient(d38wing, airfoil_db)%0A%0A    #TODO: check value

add pseudo test for mean aero moments