Zobrazeno 1 - 10
of 62
pro vyhledávání: '"Zun Cai"'
Publikováno v:
Energies, Vol 13, Iss 18, p 4801 (2020)
Effects of additional cavity floor injection on the ethylene ignition and combustion processes in a cavity-based scramjet combustor are investigated experimentally in a Mach 2.0 supersonic flow using flame luminosity and CH* (CH radical) spontaneous
Externí odkaz:
https://doaj.org/article/546feb4cab344004b8df43bb2c48a395
Publikováno v:
AIAA Journal. Mar2024, Vol. 62 Issue 3, p915-927. 13p.
Autor:
Taiyu Wang, Zhenguo Wang, Zun Cai, Mingbo Sun, Hongbo Wang, Yongchao Sun, Yixin Yang, Peibo Li, Yuhui Huang
Publikováno v:
AIAA Journal. 60:4544-4565
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6cddcdba3682798f349ab56626aed0fb
https://doi.org/10.2514/1.j061514
https://doi.org/10.2514/1.j061514
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 237:741-747
This study experimentally investigated the combustion process in a cavity-based supersonic combustor at the inflow condition of Mach 2.92 with stagnation pressure 2.6 MPa and stagnation temperature 1530 K. Time-averaged flame distribution and oscilla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9a8e7b9b38205057b0c4b1354e4d8d04
https://doi.org/10.1177/09544100221107248
https://doi.org/10.1177/09544100221107248
Publikováno v:
Chinese Journal of Aeronautics.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::623ca6ea0b332f03c9ecf5d64d0aa842
https://doi.org/10.1016/j.cja.2023.03.006
https://doi.org/10.1016/j.cja.2023.03.006
Publikováno v:
Chinese Journal of Aeronautics.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8f4d2bc4b15674ee985cb55ae1d33f9
https://doi.org/10.1016/j.cja.2023.03.010
https://doi.org/10.1016/j.cja.2023.03.010
Publikováno v:
International Journal of Hydrogen Energy. 46:26607-26615
Due to the high-speed of the air stream, the scramjet combustion is neither uniform nor complete. An empirical fuel distribution model is developed to describe non-uniform combustion for scramjet engines. The combustor is subdivided into different re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d81f9dc276190b3d90638eb2191ed650
https://doi.org/10.1016/j.ijhydene.2021.05.127
https://doi.org/10.1016/j.ijhydene.2021.05.127
Autor:
Yifu Tian, Jiajian Zhu, Mingbo Sun, Hongbo Wang, Yuhui Huang, Rong Feng, Bo Yan, Yongchao Sun, Zun Cai
Publikováno v:
Proceedings of the Combustion Institute.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bac67ebeb78df796533fb8edb5e179a6
https://doi.org/10.1016/j.proci.2022.07.101
https://doi.org/10.1016/j.proci.2022.07.101
Publikováno v:
Acta Astronautica. 182:13-20
Rocket-ejector system as a pressurization unit is of critical importance to the rocket-based combined-cycle engine under the low flight Mach number conditions. Due to the restriction of engine scale, an insufficient mixing process exists in the limit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::416bea2b3587b0c3b4429bf051a04355
https://doi.org/10.1016/j.actaastro.2021.01.055
https://doi.org/10.1016/j.actaastro.2021.01.055
Publikováno v:
Chinese Journal of Aeronautics, Vol 34, Iss 5, Pp 684-690 (2021)
The combustion modes in two different scramjet combustors with the mass flow rates of 1.8 kg/s and 3.6 kg/s are experimentally investigated to explore the scaling effects on supersonic combustion with a Mach number 2.0 inflow. It is found that the sc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0d9af5c67303ff89f016410545d1ffed
http://www.sciencedirect.com/science/article/pii/S100093612030577X
http://www.sciencedirect.com/science/article/pii/S100093612030577X