JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64237012.pdf603.95 kB
title小型超音速ロケット実験機の遷移判定
Other TitleTransition detection of experimental supersonic transport 'NEXST-1'
Author(jpn)徳川, 直子; 郭, 東潤; 吉田, 憲司
Author(eng)Tokugawa, Naoko; Kwak, Dong-Youn; Yoshida, Kenji
Author Affiliation(jpn)宇宙航空研究開発機構; 宇宙航空研究開発機構; 宇宙航空研究開発機構
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA)
Issue Date2009-02-27
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication titleJAXA special publication: Proceedings of the 41st and 42nd JAXA Workshops on Investigation and Control of Boundar-Layer Transition
宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集(第41回・第42回)
VolumeJAXA-SP-08-006
Publication date2009-02-27
Languagejpn
eng
AbstractThe experimental validation of Natural Laminar Flow wing designed with our original CFD-based inverse design method is carried out by the flight test of an unmanned and scaled supersonic experimental airplane. To add the reliability to the validation of Natural Laminar Flow wing concept, the data analysis method and numerical prediction method is investigated and improved.
Description形態: カラー図版あり
会議: 第41回「境界層遷移の解明と制御」研究会(2007年10月4日-10月5日)
KeywordsNatural Laminar Flow, SST, Boundary layers, Transition measurement, Flight testing
Document TypeTechnical Report
JAXA Category特別資料
ISSN1349-113X
NCIDAA11984031
SHI-NOAA0064237012
Report NoJAXA-SP-08-006
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/13946


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.