The paper investigates the applicability of various turbulence models for accurate modeling the aerodynamic surface design of unmanned aerodromeless transport aircraft. The numerical results are compared with the experimental data obtained as a result of the study of the airfoil section on an air test bench.
Simulation of Flows at Low Reynolds Numbers as Applied to the Design of Aerodynamic Surfaces for Unmanned Aerial Vehicles
Russ. Aeronaut.
Russian Aeronautics ; 64 , 4 ; 620-629
2021-10-01
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Aerodynamic testing at low Reynolds numbers
AIAA | 1987
|AERODYNAMIC MEASUREMENTS AT LOW REYNOLDS NUMBERS
AIAA | 1982
|