Zobrazeno 1 - 10
of 26
pro vyhledávání: '"Chen-Yuan Bai"'
Autor:
Chen-Yuan Bai, Zi-Niu Wu
Publikováno v:
Fluids, Vol 6, Iss 9, p 313 (2021)
The Mach stem height is an important parameter in the Mach reflection of steady supersonic flow. Various experimental, numerical, and theoretical works have been conducted to study this parameter in the past. However, much of the established work foc
Externí odkaz:
https://doaj.org/article/7f8a75c0d7f448eba4917f3af82d1dd6
Publikováno v:
Entropy, Vol 19, Iss 2, p 56 (2017)
The scale, inflexion point and maximum point are important scaling parameters for studying growth phenomena with a size following the lognormal function. The width of the size function and its entropy depend on the scale parameter (or the standard de
Externí odkaz:
https://doaj.org/article/d69079e12ac24d3fbaf3b5c7de40aec4
Publikováno v:
AIAA Journal. 59:282-296
Linear and nonlinear models have been studied in the past for supersonic starting flow due to forward step motion of an airfoil where the airfoil gains an angle of attack. This Paper considers the ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3c3aca5a9a84cd836d8b65f129aa30bb
https://doi.org/10.2514/1.j059199
https://doi.org/10.2514/1.j059199
Autor:
Chen-Yuan Bai, Zi-Niu Wu
Publikováno v:
Journal of Fluid Mechanics. 941
Type IV shock interference has two triple points which produce two sliplines, forming a narrow jet that penetrates into the subsonic flow region behind the bow shock. Type IV shock interference in the case that the jet is supersonic has been extensiv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::61e001c7de64c3229ebdca64e985b372
https://doi.org/10.1017/jfm.2022.340
https://doi.org/10.1017/jfm.2022.340
Publikováno v:
Acta Mechanica. 231:2125-2141
Supersonic flows around diamond airfoils, under large-amplitude step motion, are analytically studied. Nine regions with distinct flow structures are identified on each side. These regions include intricate wave structures and significantly shape the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b0ea6d04bfca92c75799c8924fd53e7
https://doi.org/10.1007/s00707-020-02637-3
https://doi.org/10.1007/s00707-020-02637-3
Publikováno v:
AIAA Journal. 58:243-254
A plate sinking in supersonic flow rapidly with pure acceleration was shown recently to have a flow structure and force behavior similar to those caused by a large-amplitude step motion, and this f...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::af38424bb80f577f5b6b24d8b2cd5f55
https://doi.org/10.2514/1.j058707
https://doi.org/10.2514/1.j058707
Autor:
Zi-Niu Wu, Chen-Yuan Bai
Publikováno v:
Fluids
Volume 6
Issue 9
Fluids, Vol 6, Iss 313, p 313 (2021)
Volume 6
Issue 9
Fluids, Vol 6, Iss 313, p 313 (2021)
The Mach stem height is an important parameter in the Mach reflection of steady supersonic flow. Various experimental, numerical, and theoretical works have been conducted to study this parameter in the past. However, much of the established work foc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::986be9e51032aef1109acf3f9f14eec4
Publikováno v:
AIAA Journal. 57:1988-2000
The classic linear Heaslet–Lomax problem, which is concerned with the indicial response of a supersonic airfoil experiencing a sudden small step motion, was recently extended to nonlinear cases whe...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ef62e026e791c89610203b52d4e6cf77
https://doi.org/10.2514/1.j057805
https://doi.org/10.2514/1.j057805
Publikováno v:
Journal of Fluid Mechanics. 903
Mach reflection subjected to the influence of an upstream shock wave from the same side is studied here. This situation occurs when two incident shock waves induced by a double wedge reflect at the same point of the reflecting surface and when the do
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e8ebeea4b3f7070270feb3f3a22c63d2
https://doi.org/10.1017/jfm.2020.677
https://doi.org/10.1017/jfm.2020.677
Publikováno v:
Journal of Fluid Mechanics. 855:882-909
Mach reflection in steady supersonic flow with two incident shock waves is studied. The second incident shock wave is produced by an additional deflection of the wedge lower surface, at some point ensuring that the two incident shock waves would inte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2bba99c647c4c2969b5fb2f9b98ba95d
https://doi.org/10.1017/jfm.2018.676
https://doi.org/10.1017/jfm.2018.676