[sam15]

I am doing a 3d wing analysis
of a wing with chord 30 cm and span 40 cm . I have completed the
meshing in gambit now i want ot do analysis in fluent.
My flow speed is 50 m/sec, RE= 1.01* 10^6(turbulent flow). please tell me the
1- which solver i use??
2-which viscous model??
3- boundary conditions ??
4- how do we get the lift and drag values in fluent after iteration??

I am a basic user . I will be thankful to u.