Zobrazeno 1 - 10
of 299
pro vyhledávání: '"Xisheng Luo"'
Publikováno v:
Aerospace, Vol 11, Iss 7, p 553 (2024)
Conventional forward bleed slots reduce the hypersonic inlet starting Mach number but suffer from excessive flow leakage after restart. This paper proposes a novel reverse bleed slot design method for curved axisymmetric inlets of a solid-fuel scramj
Externí odkaz:
https://doaj.org/article/d53f96688daf44a9a7ab4e532819854e
Publikováno v:
Journal of Fluid Mechanics; 5/25/2024, Vol. 987, p1-12, 12p
Publikováno v:
Journal of Fluid Mechanics; 2/10/2024, Vol. 980, p1-27, 27p
Publikováno v:
Journal of Fluid Mechanics; 6/25/2023, Vol. 965, p1-25, 25p
Publikováno v:
Theoretical and Applied Mechanics Letters, Vol 6, Iss 5, Pp 222-225 (2016)
The influence of high temperature effects on the protrusion of Mach stem in strong shock reflection over a wedge was numerically investigated. A two-dimensional inviscid solver applies finite volume method and unstructured quadrilateral grids were em
Externí odkaz:
https://doaj.org/article/3c7f086fc9f244398d6aac90dd10fac2
Publikováno v:
Theoretical and Applied Mechanics Letters, Vol 6, Iss 5, Pp 226-229 (2016)
The Richtmyer–Meshkov instability of a ‘V’ shaped air/helium gaseous interface subjected to a weak shock wave is experimentally studied. A soap film technique is adopted to create a ‘V’ shaped interface with accurate initial conditions. Fiv
Externí odkaz:
https://doaj.org/article/749d4c458fe4472c930bb4288eeff850
Publikováno v:
Journal of Fluid Mechanics. 959
Experiments on divergent Richtmyer–Meshkov (RM) instability at a heavy gas layer are performed in a specially designed shock tube. A novel soap-film technique is extended to generate gas layers with controllable thicknesses and shapes. An unperturb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f97e533237ff7b66a313e3a7045b2748
https://doi.org/10.1017/jfm.2023.161
https://doi.org/10.1017/jfm.2023.161
Publikováno v:
Journal of Fluid Mechanics. 956
‘Freeze-out’ of amplitude growth, i.e. the amplitude growth stagnation of a shocked helium–air interface, is realized through a reflected shock, which produces baroclinic vorticity of the opposite sign to that deposited by the first shock. Theo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::484a6d345d17fd12bb70deb5a962c0e9
https://doi.org/10.1017/jfm.2023.9
https://doi.org/10.1017/jfm.2023.9
Autor:
Yu Liang, Xisheng Luo
Publikováno v:
Journal of Fluid Mechanics. 955
Shock-induced instability developments of two successive interfaces have attracted much attention, but remain a difficult problem to solve. The feedthrough and reverberating waves between two successive interfaces significantly influence the hydrodyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea00d9a6d2b9553889651d8f7b480d0d
https://doi.org/10.1017/jfm.2023.3
https://doi.org/10.1017/jfm.2023.3
Publikováno v:
Journal of Fluid Mechanics. 953
Richtmyer–Meshkov instability induced by two successive shock waves is experimentally studied in a specific shock tube. To create two successive shock waves synchronously, a driver section is added between the driver and driven sections of the stan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::618d0fdc502ef33357aca725d6894ec1
https://doi.org/10.1017/jfm.2022.945
https://doi.org/10.1017/jfm.2022.945