Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Xiaoge Lu"'
Publikováno v:
Chinese Journal of Aeronautics. 36:190-200
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0c990969355d322f94afd8d2808f75fc
https://doi.org/10.1016/j.cja.2022.11.011
https://doi.org/10.1016/j.cja.2022.11.011
Publikováno v:
Chinese Journal of Aeronautics. 35:89-101
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b4588b2cc9e03d38de762765f6ca1348
https://doi.org/10.1016/j.cja.2022.04.014
https://doi.org/10.1016/j.cja.2022.04.014
Publikováno v:
Results in Mathematics. 78
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::19d45bfed67ae8cee55f5b53c3b47d00
https://doi.org/10.1007/s00025-022-01787-1
https://doi.org/10.1007/s00025-022-01787-1
Publikováno v:
Acta Mechanica Sinica. 38
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e617afde0ac6eaf785ee682b50448cd
https://doi.org/10.1007/s10409-022-21551-x
https://doi.org/10.1007/s10409-022-21551-x
Publikováno v:
Chinese Journal of Aeronautics, Vol 34, Iss 1, Pp 148-162 (2021)
In order to apply the air fin successfully and ensure the maneuverability of hypersonic vehicle, a key problem to be studied urgently is the heat flux brought by the fin mounting gap. The appearance of mounting gap and fin shaft can induce many compl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f47fc26e073aba4b6bd72983da7a0ed5
https://doi.org/10.1016/j.cja.2020.09.050
https://doi.org/10.1016/j.cja.2020.09.050
Publikováno v:
Experimental Thermal and Fluid Science. 141:110786
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::850ebe2b6f1a89aa18296c7a9c9373e3
https://doi.org/10.1016/j.expthermflusci.2022.110786
https://doi.org/10.1016/j.expthermflusci.2022.110786
Publikováno v:
AIAA Journal. 57:5566-5574
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3a6dc58ddf3caf168d9b8df330980b3
https://doi.org/10.2514/1.j058576
https://doi.org/10.2514/1.j058576
Delaying hypersonic boundary layer transition using forward-facing step arrays: An experimental work
Publikováno v:
Physics of Fluids. 34:065128
Our previous research has demonstrated that a single forward-facing step (FFS) could delay the hypersonic boundary layer transition on a cone [Xu et al., “Influences of steps on the hypersonic boundary-layer transition on a cone,” AIAA J. 59, 439
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ec807fa0a6af35eb731e6f0147897842
https://doi.org/10.1063/5.0094755
https://doi.org/10.1063/5.0094755
Publikováno v:
SCIENTIA SINICA Physica, Mechanica & Astronomica. 50:104706
In this paper, the interactions between shock wave and the turbulent boundary layer of an incoming wall were experimentally studied. The experiments were performed in a Mach 3.4 supersonic low-noise wind tunnel at the unit Reynolds number of 6.30×10
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c01a7b687bd732aed9c5f832444bd46b
https://doi.org/10.1360/sspma-2020-0055
https://doi.org/10.1360/sspma-2020-0055
Publikováno v:
21st AIAA International Space Planes and Hypersonics Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29b198ceb7f3624da9214c50a5d7d4d8
https://doi.org/10.2514/6.2017-2305
https://doi.org/10.2514/6.2017-2305