Abstract In this paper, simulation is considered of flow around flapped rotor sections with a degree of freedom in the flap deflection angle. For steady state validation, comparisons one made of numerical results for the flow around a flapped wing with experimental data. Modelling of a blade section with an 1-DOF aeroelastic flap is also considered.
Simulation of flow around blade section with one degree of freedom aeroelastic flap
Russian Aeronautics (Iz VUZ) ; 58 , 2 ; 193-198
01.04.2015
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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