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- W2014149712 abstract "To assist in the identification and understanding of the noise sources that contribute to the exhaust noise of aircraft gas turbine engines, controlled experiments have been carried out to study the noise characteristics of a model turbo-jet exhaust system. The noise data have been related to measurements of the aerodynamic conditions in the model and, with the aid of specific diagnostic tests, the predominant noise mechanisms are considered to have been recognized. The noise radiation, above that of the jet, is attributed primarily to dipole sources generated by the turbine outlet struts, the transmission of this noise being modified by duct propagation and nozzle impedance effects." @default.
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- W2014149712 date "1976-07-01" @default.
- W2014149712 modified "2023-09-25" @default.
- W2014149712 title "An investigation of the noise from a scale model of an engine exhaust system" @default.
- W2014149712 doi "https://doi.org/10.1016/0022-460x(76)90405-3" @default.
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