Helicopter Fuselage Wake Prediction Using Detached-Eddy Simulation

Progress in Hybrid RANS-LES ModellingNotes on Numerical Fluid Mechanics and Multidisciplinary Design(2012)

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Abstract
The capability of Detached-Eddy Simulation (DES) to predict the separated flow around a helicopter fuselage is examined and discussed. Results from two European research projects are shown: Completed simulations using a structured solver for a simplified helicopter geometry and initial results with an unstructured solver for a more complex geometry.
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Key words
Surface Pressure, Side Force, RANS Model, Prism Layer, Wind Tunnel Model
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