Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Kashiwa Wind Tunnel Working Group"'
Publikováno v:
宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :50-55
In this study, the flow characteristics of UT (University of Tokyo)-Kashiwa hypersonic wind tunnel are obtained by measuring the Pitot pressure distribution. In this wind tunnel, the Mach 7 and 9 hypersonic nozzles are inherited from its predecessor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::fe716620dfdd9bdc17c0740b21e8b804
http://id.nii.ac.jp/1696/00005609/
http://id.nii.ac.jp/1696/00005609/
