55th AIAA Aerospace Sciences Meeting 2017
DOI: 10.2514/6.2017-1217
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Use of a Ring Wing Model to investigate Factors affecting Transition Measurement using Temperature Sensitive Paint and Hot Films in Transonic Flow

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“…The particle image velocimetry (PIV) [39] technique was then used to give the velocity field information over the suction surface at the center section. Afterwards, transition locations were measured on the suction surface by the temperature sensitive paint (TSP) technique [12] [40]. Only the middle one third of the wing was painted by TSP.…”
Section: Experimental Measurementsmentioning
confidence: 99%
“…The particle image velocimetry (PIV) [39] technique was then used to give the velocity field information over the suction surface at the center section. Afterwards, transition locations were measured on the suction surface by the temperature sensitive paint (TSP) technique [12] [40]. Only the middle one third of the wing was painted by TSP.…”
Section: Experimental Measurementsmentioning
confidence: 99%