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- W1966962384 abstract "In the present comparative study of aircraft interior noise levels due to airborne and structureborne paths for a given propeller source, a structure model is used that treats the fuselage interior as a rectangular cavity with five rigid walls; the sixth, or fuselage sidewall, is a stiffened panel. The wing is modeled as a simple beam carried into the fuselage by a large, discrete stiffener representing the carry-through structure. Comparisons are made on the basis of interior noise over a range of propeller rotational frequencies at a fixed thrust. It is found that the relative importance of the structural and airborne paths is highly dependent on the structural parameters." @default.
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- W1966962384 date "1986-07-09" @default.
- W1966962384 modified "2023-09-27" @default.
- W1966962384 title "A comparison of the structureborne and airborne paths for propfan interior noise" @default.
- W1966962384 doi "https://doi.org/10.2514/6.1986-1863" @default.
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