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Enhancement and Application of the Flow Solver FLOWer

Felix Frey (), Johannes Herb, Johannes Letzgus (), Pascal Weihing (), Manuel Keßler () and Ewald Krämer ()
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Felix Frey: Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart
Johannes Herb: Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart
Johannes Letzgus: Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart
Pascal Weihing: Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart
Manuel Keßler: Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart
Ewald Krämer: Institute of Aerodynamics and Gas Dynamics (IAG), University of Stuttgart

A chapter in High Performance Computing in Science and Engineering ' 18, 2019, pp 323-336 from Springer

Abstract: Abstract Recent enhancements and applications of the flow solver FLOWer are presented in this paper. A locally formulated laminar-turbulent transition model is implemented and used for simulations of a steady and pitching finite wing. Corresponding experimental results show good agreement on transition points. In CFD, a separation bubble is observed that triggers laminar-turbulent transition. Furthermore, the paper focuses on CFD simulations conducted on Airbus Helicopters’ compound helicopter RACER and the underlying setup, including flexible main rotor blades, engine boundary conditions and deformable flaps. Finally, interaction phenomena and interesting flow characteristics are described for hovering and cruise conditions.

Date: 2019
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-030-13325-2_20

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DOI: 10.1007/978-3-030-13325-2_20

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