50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2012
DOI: 10.2514/6.2012-1187
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Transition Detection on Rotating Propeller Blades by Means of Temperature Sensitive Paint

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Cited by 29 publications
(12 citation statements)
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“…One rotor blade was coated with Ru-phen-based temperature-sensitive paint. This TSP has a short fluorescent lifetime of 0.6 μs at 303 K and high temperature sensitivity of −2.5 %/°C at 303 K (Yorita et al 2012). The Ru-phen luminophore has excitation and peak emission wavelengths of 450 and 580 nm, respectively.…”
Section: Methodsmentioning
confidence: 98%
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“…One rotor blade was coated with Ru-phen-based temperature-sensitive paint. This TSP has a short fluorescent lifetime of 0.6 μs at 303 K and high temperature sensitivity of −2.5 %/°C at 303 K (Yorita et al 2012). The Ru-phen luminophore has excitation and peak emission wavelengths of 450 and 580 nm, respectively.…”
Section: Methodsmentioning
confidence: 98%
“…Synchronization of the mirror and the rotor blade has been maintained by means of an encoder signal (200/rev) fed into the controller of the rotating mirror stepper motor (requiring 400/rev). By this technique, we are able to achieve a camera exposure time of 300 µs, which is significantly larger than that used in the earlier investigations (e.g., Yorita et al 2012).…”
Section: Blur Avoidance By Rotating Mirrormentioning
confidence: 93%
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