For a given geometry, find the aerodynamic Moment coefficient and its parameters by applying Buck$$ngham $P_1$ theorem for the aerodynam$$c moment. $($S$$k$$amaz ak$$ala verilmi$$ bir geometri i$$in Buckingham Pi teoremini aerodinamik moment i$$in uygulayarak aerodinamik moment katsay$$s$$n$$ ve parametrelerini bulunuz.$)$

Physical quantities; $($Fiziksel b$$y$$kl$$kler$)(N=6)$

$R$ Aerodvnamic Force $($Aerodvnamic Force $[$MLT$-2]$

Po density$($yo$$unluk$)[[$:$M{L}^{-3}\}$

D Length $($Uzunluk$)[$L$],$

V $-$ Speed $($Hiz$)[$LT$-1]$

$H-$ Viscosity $($Viskozite$)[$ML $[$:$L^{-1}{T}^{-1}\}$

ax Speed of Sound $($Ses nizi$)[$LT$\text{'}[$:${?}^2\}$