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- W2086256601 abstract "Accurate prediction of the rotor and fuselage interaction is essential for the design and analysis of modern rotorcraft. A variety of Navier-Stokes based methodologies have been employed in the past to simulate these effects. The purpose of this study is to examine the merits of some of the simplified techniques of modeling the rotor and their influence on the physics of the overall rotor/fuselage interaction problem. Specifically, a constant actuator disk, varying actuator disk, and blade element actuator disk are considered. The computational results are compared with wind tunnel data obtained on various rotorcraft models. The constant actuator disk is found to be inadequate for most applications, but can be easily improved upon by allowing for pressure variations about the blade radius and azimuth." @default.
- W2086256601 created "2016-06-24" @default.
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- W2086256601 date "2005-01-10" @default.
- W2086256601 modified "2023-10-18" @default.
- W2086256601 title "Analysis of Rotor-Fuselage Interactions Using Various Rotor Models" @default.
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- W2086256601 doi "https://doi.org/10.2514/6.2005-468" @default.
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