Zobrazeno 1 - 10
of 231
pro vyhledávání: '"Sadatake TOMIOKA"'
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Science. 2023, Vol. 66 Issue 3, p83-89. 7p.
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 71:12-25
Publikováno v:
CEAS Space Journal.
JAXA is conducting a flight-ground test comparison program to clarify the “facility effect” on hypersonic aerodynamics and combustion phenomena and to develop a CFD tool for predicting flight data from ground test data. The aim is a flight experi
Autor:
Yasuhiro HIGUCHI, Kiyonori TAKEUCHI, Yoshio NUNOME, Sadatake TOMIOKA, Kazuki SAKAKI, Taku KUDO, Akihiro HAYAKAWA, Hideaki KOBAYASHI
Publikováno v:
Journal of Thermal Science and Technology, Vol 14, Iss 2, Pp JTST0018-JTST0018 (2019)
This study focuses on the application of OH planar laser-induced fluorescence (OH-PLIF) in high-pressure rocket combustion conditions, up to 7.0 MPa. The signal to noise ratio of PLIF degrades in high-pressure combustion owing to effects such as line
Externí odkaz:
https://doaj.org/article/1129960dcb5847c7bcc7d05627ba32eb
Publikováno v:
CEAS Space Journal.
CHEMKIN-Pro was used to build a custom-made reduced reaction mechanism for a 3D simulation of C2H4/Air reaction in a supersonic combustion ramjet (scramjet) combustor for the JAXA S-520-RD1 flight test performed on 24 July 2022. It was also attempted
Publikováno v:
Transactions of the Japan Society for Aeronautical and Space Sciences. 65(1):33-43
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2021-06-14
資料番号: PA2210041000
Physical characteristics: Original contains color illustrations
Accepted: 2021-06-14
資料番号: PA2210041000
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Science; 2023, Vol. 66 Issue 4, p103-117, 15p
Autor:
Kiyonori TAKEUCHI, Yoshio NUNOME, Sadatake TOMIOKA, Takeo TOMITA, Taku KUDO, Akihiro HAYAKAWA, Hideaki KOBAYASHI
Publikováno v:
Journal of Thermal Science and Technology, Vol 13, Iss 1, Pp JTST0001-JTST0001 (2018)
High temperature flames, which can be produced via oxygen-enriched combustion, potentially have improved the combustion characteristics over air-only combustion flames due to their substantially higher flame temperatures. These conditions necessitate
Externí odkaz:
https://doaj.org/article/d40c179b20d34d6e9d638c3fff57e51b
Publikováno v:
Journal of Fluid Science and Technology, Vol 11, Iss 4, Pp JFST0022-JFST0022 (2016)
Measurement technique that can be adapted to high temperature and pressure environment in the rocket combustion chamber has been limited to qualitative. Therefore, establishment of a quantitative measurement technique of rocket combustion is demanded
Externí odkaz:
https://doaj.org/article/38460eadd19b407c9c945c1617994bac
Autor:
Susumu Hasegawa, Kan Kobayashi, Sadatake Tomioka, Taro Shimizu, Masatoshi Kodera, Junya Aono, Toshihiko Munakata, Masahiro Takahashi
Publikováno v:
Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan. 19(3):415-423
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2020-06-15
資料番号: PA2110054000
Physical characteristics: Original contains color illustrations
Accepted: 2020-06-15
資料番号: PA2110054000