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- W2359104322 abstract "Based on the Navier-Stokes equation in CFD,the aerodynamic interaction flow fields between the paralleled twin and triple blades are simulated to investigate the aerodynamic interaction mechanism between the helicopter rotor blades in hover.Furthermore,the aerodynamic interaction flow fields of rotor blades in hover are respectively simulated in the case of two kinds of balde number,two kinds of attack angle and two kinds of Mach number to compare and analyze their influence on the aerodynamic performance and interaction.Some valuable conclusions are given for the engineering practice." @default.
- W2359104322 created "2016-06-24" @default.
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- W2359104322 date "2007-01-01" @default.
- W2359104322 modified "2023-09-26" @default.
- W2359104322 title "On Navier-Stokes equation-based aerodynamic interaction between rotor blades in hover phase" @default.
- W2359104322 hasPublicationYear "2007" @default.
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