Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Kiyoshi Nojima"'
Publikováno v:
Journal of Fluid Science and Technology, Vol 11, Iss 1, Pp JFST0006-JFST0006 (2016)
For the next generation space launch vehicle, fully reusable spaceplane with rocket and ramjet combined propulsion system is proposed. That type of spaceplane can drastically reduce the cost per unit mass of the payload. One of the main technical cha
Externí odkaz:
https://doaj.org/article/bf6df619bdd14b79a2700ec13cc5ba3f
Autor:
Takuya ARAKAWA1 arakawa@scrj.mech.tohoku.ac.jp, Kiyoshi NOJIMA1, Kan KOBAYASHI2, Sadatake TOMIOKA2, In-Seuck Jeung
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Science. 2021, Vol. 64 Issue 2, p71-81. 11p.
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed6e8f04a9144ff83c56fb8a4c1d4e3f
https://doi.org/10.2514/6.2018-4777
https://doi.org/10.2514/6.2018-4777
Publikováno v:
2018 Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9879414d6f3ab67c10a80f710df686ab
https://doi.org/10.2514/6.2018-4931
https://doi.org/10.2514/6.2018-4931
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e282de695d63ad057f816363d9c9104
https://doi.org/10.2514/6.2016-4757
https://doi.org/10.2514/6.2016-4757
Autor:
Kiyoshi Nojima, Kouichiro Tani, Takuya Arakawa, Sadatake Tomioka, Masahiro Takahashi, Kan Kobayashi
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::53207b7a3d3d9ef38459e939ede64af1
https://doi.org/10.2514/6.2016-4758
https://doi.org/10.2514/6.2016-4758
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06651763780675288f4d061238ac59bc
https://doi.org/10.2514/6.2016-4756
https://doi.org/10.2514/6.2016-4756
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Dual-mode operation within a scramjet combustor is an efficient way to increase thrust level in supersonic regime, with little weight and thermal penalty if choking condition can be achieved thermally. To attain high thrust level in wide operation ra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc29af7a08b36b136e0b6096f4805f0e
https://doi.org/10.2514/6.2015-4142
https://doi.org/10.2514/6.2015-4142
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Experiments and a quasi-one-dimensional equilibrium calculation were conduced to estimate performances of a dual-mode combustor with ethylene fuel injection in a directconnect wind-tunnel facility in JAXA Kakuda Space Center (JAXA-KSPC). In the facil
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cdebb44509b52edcdc91f2eb77771d63
https://doi.org/10.2514/6.2014-3943
https://doi.org/10.2514/6.2014-3943
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
Three-component velocity distributions in a rocket-ramjet combined cycle engine model operating under a sea-level static condition were measured with a stereoscopic particle image velocimetry. The engine model had two rocket nozzles on top wall side
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fbbfd42a0eebad315adbd8a7c5bd91b7
https://doi.org/10.2514/6.2012-5838
https://doi.org/10.2514/6.2012-5838