Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Miaosheng, He"'
Publikováno v:
AIP Advances, Vol 14, Iss 11, Pp 115206-115206-20 (2024)
The shock train self-excited oscillation can induce combustor instabilities and reduce engine margin. In a dual-mode scramjet, the shock train undergoes a complete evolution process, exhibiting structural changes closely tied to this inherent unstead
Externí odkaz:
https://doaj.org/article/a3c6bb6d6e654af1b514440f6b6b8b02
Publikováno v:
In Procedia Engineering 2015 99:1531-1542
Publikováno v:
In Procedia Engineering 2015 99:840-847
Publikováno v:
Acta Astronautica. 187:384-393
Stable and efficient mass exchange is crucial to the combustion stability of a dual-mode scramjet. In subsonic mode, the progression of mass exchange between the cavity fluid and the mainstream, which is controlled by the cavity shear layer, is diffe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1de6ff20370a13ae0c0a17a780667716
https://doi.org/10.1016/j.actaastro.2021.06.050
https://doi.org/10.1016/j.actaastro.2021.06.050
Publikováno v:
AIAA Journal. :1-18
Multidimensional numerical simulations are performed to investigate the evolution and formation of unburned fuels for a shock–fuel jet interaction scenario. A full set of Navier–Stokes equations wi...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7b72c37ecb26ca965763f507fddb504
https://doi.org/10.2514/1.j060168
https://doi.org/10.2514/1.j060168
Publikováno v:
Applied Mathematics and Mechanics. 42:387-404
The underlying effect of vortex interaction characterized by the merging and non-merging on mixing enhancement is of fundamental significance to understand the flow dynamics of strut injectors in scramjets. Starting from a simplified configuration of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf1b436d61609b77104428dd7a4bb43d
https://doi.org/10.1007/s10483-021-2711-5
https://doi.org/10.1007/s10483-021-2711-5
Publikováno v:
Journal of Visualization. 24:19-28
The investigation of the coupling relationship between mixing enhancement and convective stretching bears practical and scientific significance. In this paper, Lagrangian perspective is adopted for compressible vortex interaction visualization to emp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6dac67715bbcb342bfb5ae9d642fbdb3
https://doi.org/10.1007/s12650-020-00698-z
https://doi.org/10.1007/s12650-020-00698-z
Publikováno v:
Combustion and Flame. 208:351-363
Molecular simulations of reacting shock-bubble interaction were performed to study viscous effects on the supersonic premixed combustion, using the Direct Simulation Monte Carlo (DSMC) method. Different bubble diameters that are comparable to the thi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a828afd9986591850751f4ee7b9db06
https://doi.org/10.1016/j.combustflame.2019.07.001
https://doi.org/10.1016/j.combustflame.2019.07.001
Publikováno v:
Aerospace Systems. 2:111-118
In the present study, asymmetric supersonic expansion flow produced by an annular conical supersonic nozzle has been studied under static conditions. To understand the details of Reynolds number influence on the backpressure-induced shock–boundary
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54d26f37ec74b877c226fee0e20189db
https://doi.org/10.1007/s42401-019-00025-x
https://doi.org/10.1007/s42401-019-00025-x
Publikováno v:
Aerospace Science and Technology. 127:107688
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5dacd1437c31c4b15f905e10646925d7
https://doi.org/10.1016/j.ast.2022.107688
https://doi.org/10.1016/j.ast.2022.107688