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- W268045709 abstract "One of the achievements of the PLGrid Plus project is development of new services and tools designed for numerical prediction of aerodynamic performance and aero-acoustic signature of helicopter rotor blades. A novel approach is based on the integration and automation of all stages of a numerical simulation pre-processing, processing and post-processing within a single tool available in the HPC environment of the PL-Grid Infrastructure. A well-established set of professional commercial software packages developed by Numeca Int. and Tecplot Inc., combined with knowledge and experience, ensure high quality of the overall service. Two initial demonstrators are designed to deliver aerodynamic performance Aero-H and aero-acoustic data Aku-H for the High-Speed Impulsive HSI noise generated by the two-bladed model of a helicopter rotor in high-speed, transonic hover conditions. An Euler or RANS structured approach to numerical simulation of the flow past ai¾źhovering rotor poses many challenges for Computational Fluid Dynamics CFD. Still, the predictions of Aero-H and Aku-H correspond well with the experimental databases of Caradonna-Tung and Purcell." @default.
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- W268045709 date "2014-01-01" @default.
- W268045709 modified "2023-09-27" @default.
- W268045709 title "Aerodynamic and Aero-acoustic Analysis of Helicopter Rotor Blades in Hover" @default.
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- W268045709 doi "https://doi.org/10.1007/978-3-319-10894-0_31" @default.
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