2021
DOI: 10.1088/1361-6501/abe2be
|View full text |Cite
|
Sign up to set email alerts
|

Measurement of boundary layer transition on oscillating airfoil using cntTSP in low-speed wind tunnel

Abstract: cntTSP is a flow visualization technique that combines temperature-sensitive paint (TSP) and carbon nanotube (CNT). TSP is a sprayable temperature sensor, and CNT is used as a thin inner electric heater for the TSP. The cntTSP technique allows the visualization of the movement of the boundary layer transition on a moving airfoil. In this study, cntTSP was applied to a pitch-oscillating airfoil in a low-speed wind tunnel. Three methods were compared as methods for detecting the boundary layer transition positio… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
5
1
1

Relationship

2
5

Authors

Journals

citations
Cited by 8 publications
(3 citation statements)
references
References 34 publications
0
3
0
Order By: Relevance
“…These TSPs exhibited an exceptionally high temperature sensitivity in a range from −35 • C to 100 • C, low pressure sensitivity, and good photostability [209]. This luminescent lanthanide complex was thereupon used for the detection of boundary layer transitions [210][211][212][213][214], for skin-friction-based measurements [215,216], and for experiments under water [217,218].…”
Section: Temperature-sensitive Paintsmentioning
confidence: 99%
“…These TSPs exhibited an exceptionally high temperature sensitivity in a range from −35 • C to 100 • C, low pressure sensitivity, and good photostability [209]. This luminescent lanthanide complex was thereupon used for the detection of boundary layer transitions [210][211][212][213][214], for skin-friction-based measurements [215,216], and for experiments under water [217,218].…”
Section: Temperature-sensitive Paintsmentioning
confidence: 99%
“…Yorita et al and Ikami et al quantitatively evaluated the static and quasi-static transition points on a wing model surface in low-speed wind tunnel tests using cntTSP [14][15][16]. Moreover, Ikami et al dynamically evaluated the motion of the transition points on a pitching airfoil under low-speed conditions [17]. This study measured the transition points on an airfoil moving at a maximum frequency of 4.2 Hz.…”
Section: Introductionmentioning
confidence: 99%
“…Recently, TSP with carbon nano-tubes (CNT) thin heating layer, called cntTSP, has been developed [ 15 , 16 ]. The cntTSP has been used for the boundary layer transition measurement under various conditions, from cryogenic wind tunnels to low-speed wind tunnels [ 17 , 18 , 19 , 20 ].…”
Section: Introductionmentioning
confidence: 99%