The relation of Aerodynamic coefficients 41210 20.210 V B2 OE B205 p,0 B 2p,0 C(M,I, 6,a, A, tan x,)= OC(M=0, Br, Be, Ba, BA, tan x, d) This correction rule is Goethert RuleThe relation of Aerodynamic coefficients: 2 ,0 2 1 2 1 ˆ 2 p x p C V V C      =   = − = −   tan , ) 1 ( 0, , , , , 1 ( , , , , ,tan , ) 2                 C M A C M A p p = = 2 ,0 2 1 2 1 ˆ 2 p x p C V V C      =   = − = −   This correction rule is Goethert Rule