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.
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
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:
Joseph Salloum, Shuichi Ueda, Andrew Ridings, Masatoshi Kodera, Michael Candon, Hideaki Ogawa
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Autor:
Michael Candon, Andrew Ridings, Joseph Salloum, Masatoshi Kodera, Shuichi Ueda, Hideaki Ogawa
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.