A combined computational/experimental investigation has been conducted to determine the time-averaged interactive performance of a propeller and wing in tractor configuration at Mach 0.1 and Re=470,000, based on a wind tunnel model wing chord of 8 in. Wing angle-of-attack was varied from 0 to +13 deg, and propeller advance ratio ranged from 2.4 (windmilling) to 1.1 (maximum power). Both a semiempirical model and a vortex lattice simulation were used in the computational analysis. Good agreement has been obtained between theory and experiment.
Aerodynamic interaction between propellers and wings
01.01.1988
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aerodynamic interaction between propellers and wings
AIAA | 1989
|Aerodynamic interaction between propellers and wings
NTRS | 1989
|Aerodynamic interaction between propellers and wings
AIAA | 1988
|