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- W2328169801 abstract "A three-dimensional droplet impingement code for aircraft propellers has been developed. The code allows the modeling of propellers of arbitrary geometry in three dimensions, but is limited to modeling axi-symmetric spinner / nacelles combinations. The code was used to analyze several 3-D wind tunnel propeller-nacelle models which were experimentally studied. The code was also used to validate a theoretical relationship between two-dimensional and three-dimensional impingement efficiencies for rotating propellers. The effects of the spinner, engine nacelle geometry, contraction of the slipstream, and blade-to-blade interference on the impingement efficiency and limits of impingement were studied. Parametric studies of the effects of the advance ratio J and droplet size on the efficiencies and limits were performed." @default.
- W2328169801 created "2016-06-24" @default.
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- W2328169801 date "1998-01-12" @default.
- W2328169801 modified "2023-09-23" @default.
- W2328169801 title "Three dimensional droplet trajectory code for propellers of arbitrary geometry" @default.
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- W2328169801 doi "https://doi.org/10.2514/6.1998-197" @default.
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