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- W3185208566 abstract "An acoustic time-of-flight sensor is operated across a turbofan exhaust plume, and is calibrated to provide nozzle thrust in a ground test cell. Validation of the technique was performed on an AE3007-A1E turbofan engine at a Rolls-Royce facility in Indianapolis. Using a pneumatic horn and a set of microphones, the acoustic time-of-flight across the exhaust plume was estimated. A correlation-based approach was then used to relate the acoustic time-of-flight to the thrust produced by the engine. The thrust estimates resulting from this single-receiver approach matched load cell data within an RMS error of 1.1% full scale. The same approach was also used to estimate the thrust of a TFE731-2B engine at Virginia Tech. In that case, the estimated thrust matched load cell data to within an RMS error of 1.5% full scale." @default.
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- W3185208566 date "2021-07-28" @default.
- W3185208566 modified "2023-10-03" @default.
- W3185208566 title "Thrust Measurements using Acoustic Sensing on a Turbofan Engine Exhaust Plume" @default.
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- W3185208566 doi "https://doi.org/10.2514/6.2021-3476" @default.
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