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020 _a9789811068324
024 7 _a10.1007/978-981-10-6832-4
_2doi
040 _aES-MaUEC
_bspa
050 4 _aTL574.L3
_bR465 2018 EB
100 1 _aRen, Jie
_0http://id.loc.gov/authorities/names/nr00006460
_1http://viaf.org/viaf/4957151/
245 1 0 _aSecondary Instabilities of Görtler Vortices in High-Speed Boundary Layers
_bMechanisms and Flow Control on Laminar-Turbulent Transition
_cby Jie Ren.
264 1 _aSingapore
_bSpringer International Publishing
_c2018
300 _a1 recurso en línea (XVIII, 94 páginas 51 ilustraciones, 41 ilustraciones a color)
347 _atext file
_bPDF
490 0 _aSpringer Theses, Recognizing Outstanding Ph.D. Research
_x2190-5053
520 3 _aThis thesis first reveals the mechanism of Görtler instabilities and then demonstrates how transitions at hypersonic flows can be effectively controlled (either promoted or suppressed) with Görtler or Klebanoff modes. It focuses on understanding and controlling flow transitions from mild laminar to fully turbulent flows at high speeds-aspects that have become crucial at the dawn of an incredible era, in which hypersonic vehicles are becoming available. Once this occurs, it will be possible to travel from Beijing to Los Angeles within just 2 hours, and we will all live in a genuinely global village-and not just virtually, but physically. Görtler instabilities have often been used to promote flow transition in hypersonic vehicles. However, how Görtler instabilities are excited and how they evolve in hypersonic flows are questions that have yet to be answered.
650 7 _aFlujo laminar
_9667336
_2embne
650 7 _aIngeniería
_xModelos matemáticos
_2embne
_9667394
776 0 8 _iEdición impresa:
_z9789811068317
776 0 8 _iEdición impresa:
_z9789811068331
856 4 0 _uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-10-6832-4
_zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
490 0 _aEngineering (Springer-11647)
988 _aEBSPRINGER_2018
998 _b02/2019
_dz
_ek
_feng
_ggw
_h0
999 _c102927
_d102927
_x1