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

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title高速応答型感圧コーティングによるデルタ翼上の非定常圧力計測
Other TitleUnsteady surface pressure measurements on a delta wing by fast-responding pressure-sensitive coating
Author(jpn)川上 崇穂; 田部井 孝聡; 亀田 正治; 中北 和之; 浅井 圭介
Author(eng)Kawakami, Takaho; Tabei, Takatoshi; Kameda, Masaharu; Nakakita, Kazuyuki; Asai, Keisuke
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; 東北大学
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; Tohoku University
Issue Date2004-05
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
宇宙航空研究開発機構宇宙科学研究本部
Publication title宇宙航行の力学シンポジウム 平成15年度
Symposium on Flight Mechanics and Astrodynamics 2003
Start page31
End page34
Publication date2004-05
Languagejpn
Keywordsdelta wing; pressure sensitive paint; pressure measurement; transonic flow; wind tunnel model; shock wave interaction; leading edge; boundary layer separation; デルタ翼; 感圧塗料; 圧力測定; 遷音速流; 風洞模型; 衝撃波干渉; 前縁; 境界層剥離
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会
SHI-NOAA0047120009
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/34380


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