Pressure-Sensitive Paint Measurements in High-Speed Wind Tunnels
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- NAKAKITA Kazuyuki
- 宇宙航空研究開発機構 航空本部
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- KURITA Mitsuru
- 宇宙航空研究開発機構 航空本部
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- KAMEDA Masaharu
- 東京農工大学工学府 機械システム工学専攻
Bibliographic Information
- Other Title
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- 高速風洞試験におけるPSP計測
- コウソク フウドウ シケン ニ オケル PSP ケイソク
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Abstract
Two types of the pressure-sensitive paint measurement techniques for high-speed wind tunnels, which include transonic and supersonic ones, were introduced. They were the practical PSP measurement, whose targets were development tests of aerospace vehicles, and the unsteady PSP measurement. <br>For the practical PSP measurement, PSP/TSP paints, measurement systems, and data reduction methods were described. Then, the global PSP measurement results of the DLR-F6 model were discussed about pressure distribution and variation between those of two AoA cases. <br>For the unsteady PSP measurement, PSP paint/coating of anodized-aluminum PSP and silica nanoparticle PSP and measurement system were described, then, the unsteady PSP measurement results of the rocket faring model using AA-PSP and those of the delta wing model using silica nanoparticle PSP, whose targets were transonic buffet phenomena, were introduced.
Journal
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- Journal of the Visualization Society of Japan
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Journal of the Visualization Society of Japan 34 (132), 9-15, 2014
The Visualization Society of Japan
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Details 詳細情報について
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- CRID
- 1390001204622791552
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- NII Article ID
- 130004872112
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- NII Book ID
- AN10374478
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- DOI
- 10.3154/jvs.34.9
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- ISSN
- 1884037X
- 09164731
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- NDL BIB ID
- 025168827
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
- KAKEN
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- Abstract License Flag
- Disallowed