Fast responding pressure-sensitive paint: Accuracy improvement, combination with another measurement, and application to unsteady aerodynamics
Project/Area Number |
22360075
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Research Category |
Grant-in-Aid for Scientific Research (B)
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Allocation Type | Single-year Grants |
Section | 一般 |
Research Field |
Fluid engineering
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Research Institution | Tokyo University of Agriculture and Technology |
Principal Investigator |
KAMEDA Masaharu 東京農工大学, 大学院・工学研究院, 教授 (70262243)
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Co-Investigator(Kenkyū-buntansha) |
AMAO Yutaka 大分大学, 工学部, 准教授 (80300961)
NAKAKITA Kazuyuki 宇宙航空研究開発機構, 研究開発本部, 研究領域リーダ (50358595)
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Co-Investigator(Renkei-kenkyūsha) |
KATO Hiroyuki 宇宙航空研究開発機構, 研究開発本部, 主任研究員 (80358598)
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Project Period (FY) |
2010 – 2012
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Project Status |
Completed (Fiscal Year 2012)
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Budget Amount *help |
¥19,240,000 (Direct Cost: ¥14,800,000、Indirect Cost: ¥4,440,000)
Fiscal Year 2012: ¥2,730,000 (Direct Cost: ¥2,100,000、Indirect Cost: ¥630,000)
Fiscal Year 2011: ¥4,550,000 (Direct Cost: ¥3,500,000、Indirect Cost: ¥1,050,000)
Fiscal Year 2010: ¥11,960,000 (Direct Cost: ¥9,200,000、Indirect Cost: ¥2,760,000)
|
Keywords | 流体工学 / 航空宇宙工学 / 計測工学 / 感圧塗料 / 風洞実験 / PIV / 複合計測 / 超微粒子セラミック |
Research Abstract |
A novel method for measuring the pressure and velocity fields of unsteady flow around bodies was constructed. The measurement technique using fast responding pressure-sensitive paint (PSP) was improved to detect the pressure fluctuation whose frequency and amplitude are 5 kHz and less than 100 Pa. An analytic solution of the frequency response of the PSP signal was derived in which the effect of luminescence lifetime was considered. A coupled system using this PSP and the time-resolved particle-image velocimetry (PIV) was constructed. Wind-tunnel test of this system indicated that the sheading droplets for PIV hardly disturbed the signal from the PSP. The vorticity obtained by PIV correlated well with the pressure fluctuation measured by PSP.
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Report
(4 results)
Research Products
(34 results)
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[Presentation] Frequency response of fast-response pressure sensitive paint with a hydrophobic coating2012
Author(s)
Seya, Y., Nishida, R., Yoshida, M., Kameda, M. and Nakakita, K
Organizer
3rdJapanese-German Joint Seminar on Molecular Imaging Technology for Interdisciplinary Research
Place of Presentation
JAXA ChofuAerspace Center, Chofu, Tokyo, Japan
Year and Date
2012-09-04
Related Report
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[Presentation] Simultaneous pressure and velocity field measurement ofpseudo-shock-wave using PSP and PIV2012
Author(s)
Koike, S., Osawa, J., Nakakita, K.,Kato, H., and Kameda, M
Organizer
50th AIAA Aerospace Sciences Meeting
Place of Presentation
Gaylord Opryland Resort& Convention Center, Nashville, Tennessee, U.S.A.
Year and Date
2012-01-12
Related Report
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[Presentation] Simultaneous pressure and velocity field measurement of pseudo-shock-wave using PSP and PIV2012
Author(s)
Koike, S., Osawa, J., Nakakita, K., Kato, H., Kameda, M
Organizer
50th AIAA Aerospace Sciences Meeting
Place of Presentation
Gaylord Opryland Resort & Convention Center, Nashville, Tennessee, U.S.A
Year and Date
2012-01-12
Related Report
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[Presentation] Visualization of shock-induced vortex breakdown on a delta wing in transonic flow regime2011
Author(s)
Makoshi, T, Kashida, T., Kimura, S.,Seya, Y. and Kameda, M
Organizer
11th Asian Symposium on Visualization
Place of Presentation
Toki Messe, Niigata, Japan
Year and Date
2011-06-08
Related Report
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[Presentation] Frequency response of fast-response pressure sensitive paint with a hydrophobic coating
Author(s)
Seya, Y., Nishida, R., Yoshida, M., Kameda, M. and Nakakita, K.
Organizer
3rd Japanese-German Joint Seminar on Molecular Imaging Technology for Interdisciplinary Research
Place of Presentation
JAXA Chofu Aerospace Center, Chofu, Tokyo, Japan
Related Report
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[Presentation] 多孔質皮膜感圧塗料の時間応答性
Author(s)
亀田 正治, 瀬谷 佑介, 吉田 匡秀, 中北 和之
Organizer
第44回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム
Place of Presentation
富山国際会議場, 富山
Related Report
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