Zobrazeno 1 - 10
of 63
pro vyhledávání: '"Masatoshi Kodera"'
Autor:
Hironobu NISHIGUCHI1 a09017516373@outlook.jp, Masatoshi KODERA2, Sadatake TOMIOKA2, Nobuyuki Tsuboi
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Science. 2023, Vol. 66 Issue 4, p103-117. 15p.
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
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
Publikováno v:
AIAA Journal. 58:4819-4831
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2020-07-09
資料番号: PA2110004000
Physical characteristics: Original contains color illustrations
Accepted: 2020-07-09
資料番号: PA2110004000
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Publikováno v:
23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Publikováno v:
Journal of Propulsion and Power. 32:1110-1118
Experimental tests are conducted to evaluate the effect of an annular rocket exhaust pattern on the mixing characteristics of a simple ejector. Rocket exhaust is simulated using pure oxygen while air is entrained from the surroundings at static condi
Autor:
Sadatake Tomioka, Takeshi Tsuchiya, Takahiro Fujikawa, Tatsushi Isono, Kan Kobayashi, Masatoshi Kodera, Kouichiro Tani
Publikováno v:
Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2018-01-19
資料番号: PA1810076000
Physical characteristics: Original contains color illustrations
Accepted: 2018-01-19
資料番号: PA1810076000
Autor:
Hideaki Ogawa, Masatoshi Kodera
Publikováno v:
Journal of Propulsion and Power. 31(5):1423-1435
Efficient mixing of fuel and air is a major objective for the successful operation of scramjet engines, in which the supersonic combustion process must occur within an extremely short time frame in the hypersonic flight. This paper presents the insig
Autor:
Masahiro TAKAHASHI, Sadatake TOMIOKA, Masatoshi KODERA, Kan KOBAYASHI, Susumu HASEGAWA, Taro SHIMIZU, Junya AONO, Toshihiko MUNAKATA
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2021, Vol. 19 Issue 3, p415-423, 9p