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Showing 1 to 2 of 2 for “"Slipstream effects"”.

  1. A Numerical Vortex Approach To Aerodynamic Modeling of SUAV/VTOL Aircraft

    … a low-cost approach to preliminary modeling of slipstream effects on a finite wing. The wing aerodynamic model employs a numerical lifting-line method utilizing the 3D vortex lifting law along with known 2D airfoil data to predict the lift distribution across a wing for a prescribed upstream …

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  2. Aerodynamics of lifting surfaces in propeller slipstreams

    … airfoil with chord length of 1 ft in a propeller slipstream at a freestream Reynolds number of 100,000 are presented in this study. ANSYS FLUENT was used to solve the flow equations inside the control volume. For the two-dimensional analysis, the propeller was modeled as an actuator line across …

    uiuc Repository record for Aerodynamics of lifting surfaces in propeller slipstreams (opens in a new tab)