Script file to generate data at various angle of attack and Mach no.
 

Hello all,

I am new to Fluent and would like to automate generatation of aero-coefficients for an airfoil at various angle-of-attack and mach no, ie batch file or script. Appreciate if someone can help me on this.
Also, I can use the same mesh for desired range of angle-of-attacks just by changing the X- and Y- flow direction. And I sweep the mach number by changing the mach no at boundary far-field only. Is this correct?

Thanks!