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- W2377053871 abstract "An analytical method, which calculates the unsteady a erodynamic in teractions between the rotor and its wake and the fuselage of helicopters, is ba sed on the blade secondorder liftingline model, the rotor fullspan free wa ke model, and the fuselage source panel model. These models are coupled together to form a global analytical model by iterating on the induced velocities of the fuselage on the rotor inflow plane and collocating points of the wake as well a s the rotor and its wake on the surface of the fuselage. The unsteady term was incorporated into this analysis. As numerical examples, calculations are carrie d out on the meantime pressure distribution for two isolated fuselages and the unsteady pressure coefficient for a combined rotor/fuselage configuration. Thr ough the comparison between the calculated results and available experimental da ta, the capability of the present method is indicated." @default.
- W2377053871 created "2016-06-24" @default.
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- W2377053871 date "2000-01-01" @default.
- W2377053871 modified "2023-09-24" @default.
- W2377053871 title "Analysis of unsteady aerodynamic interactions between rotor and fuselage of helicopters in forward flight" @default.
- W2377053871 hasPublicationYear "2000" @default.
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