Biennial Flight Test Conference 1994
DOI: 10.2514/6.1994-2115
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Evaluating the dynamic response of in-flight thrust calculation techniques during throttle transients

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Cited by 4 publications
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“…Measurement data for a throttle frequency sweep maneuver [34] Page 14/17 Fuel mass ow rate estimation using the original and revised data-driven models…”
Section: Discussionmentioning
confidence: 99%
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“…Measurement data for a throttle frequency sweep maneuver [34] Page 14/17 Fuel mass ow rate estimation using the original and revised data-driven models…”
Section: Discussionmentioning
confidence: 99%
“…The ow at the LPT outlet was split into the HPC and bypass duct, and the two ows were mixed at the outlet of the LPT. For data-driven model training, measurement data from a throttle frequency sweep maneuver, as shown in Ray's study [34], were used. Figure 3 presents the LPT inlet total temperature, LP shaft speed, engine net thrust, and fuel mass ow rate during a throttle frequency sweep maneuver.…”
Section: Test Enginementioning
confidence: 99%