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pro vyhledávání: '"Tsuda, Shoichi"'
Akademický článek
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Autor:
Sasaki, Takashi, Tsuda, Shoichi, Riemer, R. Kirk, Ramamoorthy, Chandra, Reddy, V. Mohan, Hanley, Frank L.
Publikováno v:
In The Journal of Thoracic and Cardiovascular Surgery 2010 139(3):530-535
Autor:
Sugimori, Haruhiko, Nakao, Tatsuya, Ikegaya, Yuki, Iwahashi, Daisuke, Tsuda, Shoichi, Kume, Nao, Onishi, Hirokazu, Nakamura, Sunao
Additional file 1: Supplemental Table 1. Number of congenital heart disease and open-heart surgeries performed in the past 20 years. The numbers in parentheses represent the number of concomitant anomalies. The cases were as follows: one case of VSD
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0a391d29312ac674f16fbd5d2afc8d62
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Autor:
Fujii, Keisuke, Hirabayashi, Noriaki, Koyama, Tadao, Tsuda, Shoichi, Nakagawa, Muneyoshi, Itabashi, Yukihiro, Nakamura, Akiyoshi, Okabayashi, Kie, Takama, Yoshiki
Publikováno v:
宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report. :1-36
シュリーレン可視化法は高速気流観測に非常に広く使われている密度勾配に関した計測手法の一つであるが、密度勾配の観測線上にわたる積分値を与えるという性質上3次元的な流れ場に
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::4a081396492e7c10f8ebd4209a91448a
http://id.nii.ac.jp/1696/00001906/
http://id.nii.ac.jp/1696/00001906/
Autor:
Sasaki, Takashi1 (AUTHOR) tsasaki3@stanford.edu, Tsuda, Shoichi1 (AUTHOR), Trujillo, Mario1 (AUTHOR), Kirk Riemer, R.1 (AUTHOR), Reinhartz, Olaf1 (AUTHOR)
Publikováno v:
Journal of Investigative Surgery. Feb2012, Vol. 25 Issue 1, p29-32. 4p.
Autor:
Fujii, Keisuke, Hirabayashi, Noriaki, Koyama, Tadao, Tsuda, Shoichi, Nakamura, Akihiro, Watari, Minoru, Taguchi, Hideyuki
Publikováno v:
宇宙航空研究開発機構特別資料: 第80回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Technology Association 80th meeting. :16-21
第80回風洞研究会議(2008年5月15日-5月16日）
近年の極超音速領域の対象として注目されている極超音速機をはじめとする細長形状・低迎角極超音速飛行体に関する風洞試験において，
近年の極超音速領域の対象として注目されている極超音速機をはじめとする細長形状・低迎角極超音速飛行体に関する風洞試験において，
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::3ae9e71685a5aa64fc8e475115614a50
http://id.nii.ac.jp/1696/00005154/
http://id.nii.ac.jp/1696/00005154/
Autor:
Tsuda, Shoichi, Koyama, Tadao, Hirabayashi, Noriaki, Watari, Minoru, Sekine, Hideo, Kibushi, Junko, Nakamura, Akiyoshi
Publikováno v:
宇宙航空研究開発機構特別資料: 第78回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 78th Meeting. :33-39
Force tests were carried out using an AGARD-B calibration model in the JAXA 0.5 m Hypersonic Wind Tunnel (HWT1) at a nominal Mach number of 5. The aerodynamic characteristics of the AGARD-B calibration model were obtained successfully. The experiment
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::336e9d935d66d52bf2fc08858bd15eba
http://id.nii.ac.jp/1696/00005675/
http://id.nii.ac.jp/1696/00005675/
Autor:
Kuchiishi, Shigeru, Watanabe, Shigeya, Nagai, Shinji, Tsuda, Shoichi, Koyama, Tadao, Hirabayashi, Noriaki, Sekine, Hideo, Hozumi, Koichi
Publikováno v:
宇宙航空研究開発機構特別資料: 第74回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 74th Meeting. :48-52
In the present paper, results of force and heat flux measurement tests conducted in the JAXA 1.27 m Hypersonic Wind Tunnel (HWT) using the HB-2 standard model are presented. The tests were conducted at a nominal Mach number of 10, a stagnation enthal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::6adca98e4b4097754786d05eb6afa2c2
http://id.nii.ac.jp/1696/00006173/
http://id.nii.ac.jp/1696/00006173/
Autor:
Tsuda, Shoichi, Watari, Minoru
Publikováno v:
宇宙航空研究開発機構特別資料: 第75回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 75th Meeting. :17-21
Comprehensive HB-2 standard model tests are underway in the hypersonic wind tunnels in JAXA. The HB-2 force/moment test in Mach 10 flow was conducted in the 0.44 m Hypersonic Shock Tunnel (HST) with a new model support system. Vibration acceleration
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::207b857af3dd045861912967c6614cb3
http://id.nii.ac.jp/1696/00006119/
http://id.nii.ac.jp/1696/00006119/