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- W2313305892 abstract "In this study, the effect of a propeller slipstream on the aerodynamics of an UAV was investigated. For this purpose, an actuator disk model was implemented into an in-house Computational Fluid Dynamics (CFD) solver. To validate the model, available data from an experiment 2 that was performed for a simple nacelle with and without wing was used. The measured and computed pressure distributions over the nacelle and the wings were compared and satisfactory results were obtained. Finally, the implemented model was used to generate the main aerodynamic coefficients of an aft-propelled UAV." @default.
- W2313305892 created "2016-06-24" @default.
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- W2313305892 date "2013-06-22" @default.
- W2313305892 modified "2023-09-25" @default.
- W2313305892 title "Implementation and Validation of an Actuator Disk Model for Aerodynamic Analysis of Propelled UAVs" @default.
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- W2313305892 doi "https://doi.org/10.2514/6.2013-3047" @default.
- W2313305892 hasPublicationYear "2013" @default.
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