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- W1492405934 abstract "In order to numerically determine the laminar-turbulent transition on hovering rotors, the applicability of three different prediction methods originating from fixed wing applications has been investigated. This includes the AHD method, used with approximated boundary layer data, and the Drela eN envelope method, using integral boundary layer parameters. Both methods are implemented in the structured flow solver FLOWer. Furthermore, a boundary layer / eN stability code coupled to the hybrid flow solver TAU was taken into account. One two-dimensional test case (Somers airfoil) and two three-dimensional hovering rotor test cases (ONERA 7A rotor and DLR Bo 105 flight test) serve to test and validate predicted transition and its influence on rotor performance." @default.
- W1492405934 created "2016-06-24" @default.
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- W1492405934 date "2010-09-01" @default.
- W1492405934 modified "2023-09-27" @default.
- W1492405934 title "Accurate Numerical Flow Simulation of Hovering Rotors using different Transition Prediction Methods" @default.
- W1492405934 hasPublicationYear "2010" @default.
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