JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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Other TitleQuantitative measurement of unsteady pressure field on a delta wing by means of a fast-response PSP
Author(jpn)田部井 孝聡; 川上 崇穂; 亀田 正治; 中北 和之
Author(eng)Tabei, Takatoshi; Kawakami, Takaho; Kameda, Masaharu; Nakakita, Kazuyuki
Author Affiliation(jpn)東京農工大学; 東京農工大学; 東京農工大学; 宇宙航空研究開発機構
Author Affiliation(eng)Tokyo University of Agriculture and Technology; Tokyo University of Agriculture and Technology; Tokyo University of Agriculture and Technology; Japan Aerospace Exploration Agency
Issue Date2005-03
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
Publication title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
Start page128
End page131
Publication date2005-03
Keywordspressure measurement; unsteady aerodynamics; delta wing; pressure sensitive paint; unsteady pressure field; shock tube; transonic wind tunnel; wind tunnel test; flow visualization; 圧力測定; 非定常空力学; デルタ翼; 感圧塗料; 非定常圧力場; 衝撃波管; 遷音速風洞; 風洞試験; 流れの可視化
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

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