Zobrazeno 1 - 10
of 17
pro vyhledávání: '"ChangFei Zhuo"'
Publikováno v:
Symmetry, Vol 12, Iss 4, p 518 (2020)
The reason for the asymmetry phenomenon of Shock/Boundary Layer Interactions (SBLI) in a completely symmetric duct with symmetric flow conditions is still an open question. A theoretical model for the asymmetry of shock train in supersonic flows is p
Externí odkaz:
https://doaj.org/article/968f954cf17f4789b1fc77e262a710bc
Publikováno v:
Acta Astronautica. 193:237-254
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::863b218830df533a45898e7b7fbecdcd
https://doi.org/10.1016/j.actaastro.2022.01.013
https://doi.org/10.1016/j.actaastro.2022.01.013
Publikováno v:
Fuel. 326:125088
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45cc8b6d568ff23614a9744dabf842fd
https://doi.org/10.1016/j.fuel.2022.125088
https://doi.org/10.1016/j.fuel.2022.125088
Publikováno v:
Experimental Thermal and Fluid Science. 103:364-376
A plane-radial rotating detonation engine (RDE) was tested to identify the impact of different injection conditions on the propagation mode and parameters of rotating detonation wave (RDW). Changing the mass flow rate and equivalence ratio, various p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22f39eb598f547175181810d5d2b70d9
https://doi.org/10.1016/j.expthermflusci.2019.01.032
https://doi.org/10.1016/j.expthermflusci.2019.01.032
Publikováno v:
Chinese Journal of Aeronautics, Vol 32, Iss 4, Pp 851-860 (2019)
To research the self-ignition characteristics of high-speed ramjet kinetic energy projectile in the launch process, the self-ignition process based on the solid fuel of polyethylene was numerically simulated by using the dynamic grid technology. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6854da8c6b6da43bbe01d715f8918e4a
https://doi.org/10.1016/j.cja.2019.01.011
https://doi.org/10.1016/j.cja.2019.01.011
Publikováno v:
Journal of Physics: Conference Series. 2235:012012
Three-dimensional numerical simulations were conducted on a non-premixed rotating detonation engine (RDE) with different exhaust nozzles (i.e. without a nozzle, with a divergent nozzle, with a convergent nozzle, and with a Laval nozzle). Aside from d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::846113d85dda349b48157ac78a0d57b8
https://doi.org/10.1088/1742-6596/2235/1/012012
https://doi.org/10.1088/1742-6596/2235/1/012012
Publikováno v:
Aerospace Science and Technology. 124:107526
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea92b2ebc23dcfff3cd1ce33e833d79f
https://doi.org/10.1016/j.ast.2022.107526
https://doi.org/10.1016/j.ast.2022.107526
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 233:2378-2392
This paper simulates the propagation characteristics of rotating detonation wave in the plane–radial structure for mixtures of 2H2 + O2 + 3.76N2. Two-dimensional numerical simulation was modeled, and two kinds of typical flow field and correspondin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41eaadc7b40e5b8dcfa09ef09fd58584
https://doi.org/10.1177/0954410018779300
https://doi.org/10.1177/0954410018779300
Publikováno v:
International Journal of Hydrogen Energy. 43:4609-4622
The rotating detonation wave (RDW) propagation processes and influence factors are simulated in the plane-radial structure. The effects of inner radii of curvature, domain widths and stagnation pressures on propagation mode are studied. The RDW is in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bda7a1fde52f3dcafa649a6490d4221d
https://doi.org/10.1016/j.ijhydene.2018.01.061
https://doi.org/10.1016/j.ijhydene.2018.01.061
Publikováno v:
Aerospace Science and Technology. 115:106786
To investigate the influence of the real-gas effect on the flow of the inward-turning inlet while an air-breathing propulsion system flies at a high Mach number, gas models of thermally perfect gas, chemical non-equilibrium gas, and thermochemical no
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::916cce28e85154dde600956081d3eef1
https://doi.org/10.1016/j.ast.2021.106786
https://doi.org/10.1016/j.ast.2021.106786