Quantitative measurement of unsteady pressure field on a delta wing by means of a fast-response PSP

Authors :: Tabei, Takatoshi
Kawakami, Takaho
Kameda, Masaharu
Nakakita, Kazuyuki
Source :: 宇宙航行の力学シンポジウム平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004. :128-131
Publication Year :: 2005
Publisher :: 宇宙航空研究開発機構宇宙科学研究本部, 2005.
Abstract: 資料番号: AA0048089033

Subjects :: delta wing
unsteady aerodynamics
unsteady pressure field
transonic wind tunnel
遷音速風洞
 shock tube
風洞試験
 pressure sensitive paint
非定常圧力場
 非定常空力学
 デルタ翼
 圧力測定
 感圧塗料
 flow visualization
衝撃波管
 pressure measurement
wind tunnel test
流れの可視化

Language :: Japanese
Database :: OpenAIRE
Journal :: 宇宙航行の力学シンポジウム平成16年度 = Symposium on Flight Mechanics and Astrodynamics 2004
Accession number :: edsair.jairo.........2c00d1b72debf7ccf8d40e80d5dc5577

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