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- W2370187016 abstract "Based on unsteady aerodynamic model,a numerical method has been given to calculate the unsteady lift and pitching moment acting on an airfoil of the rotor operating at slightly stall and deep stall conditions in compressible flow.The method was expressed as a set of semi-empirical indicial response formula,and solved by numerical discretization.As numerical examples,the normal force and pitching moment on NACA0012 and SC-1095 airfoils were calculated,and the comparisons with available experimental data were made so as to show the capability of the present method.The influence of the reduced frequency and Mach number on dynamic stall responses is also investigated.Then,the method was improved to be suitable for the calculations of dynamic stall responses in swept flow,and the swept effects on the airfoil responses were analyzed and discussed.Finally,a few conclusions were presented." @default.
- W2370187016 created "2016-06-24" @default.
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- W2370187016 date "2007-01-01" @default.
- W2370187016 modified "2023-09-23" @default.
- W2370187016 title "Computations of unsteady dynamic stall responses on rotor airfoils" @default.
- W2370187016 hasPublicationYear "2007" @default.
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