Abstract Flows around rotor blade sections equipped with active flaps with a degree of freedom in the flap deflection angle are considered in this paper. Results for oscillating flaps are presented. The resultant flap motion was found to couple with the unsteady air loads for cases of blade section in oscillatory translation.
Simulation of flow around oscillating rotor blade section with aeroelastic flap
Russian Aeronautics (Iz VUZ) ; 58 , 4 ; 419-425
2015-10-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Simulation of flow around oscillating rotor blade section with aeroelastic flap
Online Contents | 2015
|Simulation of flow around blade section with one degree of freedom aeroelastic flap
Springer Verlag | 2015
|Simulation of flow around blade section with one degree of freedom aeroelastic flap
Online Contents | 2015
|