Simulation Past NASA Rotor-35
I am not able to generate a geometry of Blade Passage between NASA Rotor-35 and import it in ANSYS to extract the sound field. If someone could provide me the Blade geometry of the same which could be imported in ANSYS and help me out in extracting the sound field past the transonic rotors it would be of great use to me.
Thanks and Regards
|All times are GMT -4. The time now is 14:53.|