34th Congress of the International Council of the Aeronautical Sciences

03.4 - Applied Aerodynamics

SIMULATION OF AN INSTALLED PROPELLER BY MEANS OF STEADY AND UNSTEADY BODY-FORCE MODELING

H. Pantel¹, F. Falissard¹, G. Dufour, ISAE-SUPAERO, France; ¹ONERA, France

Assessment of the actuator line body force method for a propeller. The results are compared to URANS blade-resolved computations, lifting line computations, and steady body force computations. The simulations include an isolated propeller case and and installed case on a wing.


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