[rishabh.cfd]

angle of attack = α
sideslip angle = β (degrees)

Want to define Boundary condition , which consist
of both α and β.
Ex: α = 10 β = 5 (degrees)

B.C. : Farfield M = 0.5 [V = 168 m/s]

X componet of velocity =
Y componet of velocity =
Z componet of velocity =

Please tell me How to define α = 10 β = 5 , For M = 0.5
in terms of Velocity component?????