|March 3, 2015, 22:58||
Script file to generate data at various angle of attack and Mach no.
Join Date: Mar 2015
Posts: 1Rep Power: 0
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?
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