2016
DOI: 10.2514/1.j054207
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Subsonic In-Flight Temperature and Pressure Measurements Using a Scramjet Inlet Flow Sensor

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Cited by 6 publications
(3 citation statements)
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“…A prototype was successfully tested on the ground for signal fluctuations and signal-to-noise ratio under the pressure, temperature, and vibration conditions expected during a hypersonic flight test. The design is significantly simpler than previous designs presented in the literature and was the first TDLAS sensor design used in a scramjet inlet during a flight test [6,7].…”
Section: Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…A prototype was successfully tested on the ground for signal fluctuations and signal-to-noise ratio under the pressure, temperature, and vibration conditions expected during a hypersonic flight test. The design is significantly simpler than previous designs presented in the literature and was the first TDLAS sensor design used in a scramjet inlet during a flight test [6,7].…”
Section: Discussionmentioning
confidence: 99%
“…This paper concerns the design, development, and ground testing of a diode-laser-based oxygen sensor for this inlet flow. Companion papers describe the flight test results [6,7].…”
Section: Introductionmentioning
confidence: 99%
“…This method is an autoregressive data-driven model based on data flow and its prediction interval, which has the characteristics of fast execution, large amount of data, and no need to classify outliers in advance. The authors in [16] briefly introduces the technical basis of NN and BPNN (backpropagation neural network). The principle and method of sensor fault diagnosis based on NN observer are discussed.…”
Section: Related Workmentioning
confidence: 99%