Please use this identifier to cite or link to this item: http://hdl.handle.net/11189/8199
DC FieldValueLanguage
dc.contributor.authorSun, BoHuaen_US
dc.contributor.authorOran, Elaine S.en_US
dc.date.accessioned2021-10-26T06:26:15Z-
dc.date.available2021-10-26T06:26:15Z-
dc.date.issued2018-
dc.identifier.citationSun, B. & Oran, E. S. 2018. New principle for aerodynamic heating. National Science Review, 5(5): 606–607. [https://doi.org/10.1093/nsr/nwy035]en_US
dc.identifier.issn2053-714X-
dc.identifier.issn2095-5138-
dc.identifier.urihttp://hdl.handle.net/11189/8199-
dc.description.abstractFluid flows that we encounter in nature are mostly turbulent. To date, the physics of turbulence has not been clear and is still considered as ‘the last unsolved problem in classical physics’. Its complex dynamical process reflects the strong nonlinearity of the Navier–Stokes equation, which is a millennium math problem.The modeling and control of developed turbulence and the onset of turbulence, i.e. transition, are still bottlenecks in engineering applications such as aeronautics, astronautics and navigation. Recently, hypersonic boundary-layer transition has become a strategic focus because of its severe impact on the aerodynamic force and heating of a highspeed vehicle. Compared to incompressible flows, hypersonic transition and its effect on aerodynamic heating are less understood owing to additional complexities such as second- and higher-order instability modes and non-linear coupling of different processes.en_US
dc.language.isoenen_US
dc.publisherChina Science Publishing & Media Ltd. (Science Press)en_US
dc.relation.ispartofNational Science Reviewen_US
dc.subjectFluid flowsen_US
dc.subjectaerodynamic heatingen_US
dc.subjectNavier–Stokes equationen_US
dc.subjectturbulenceen_US
dc.subjecthypersonic boundary-layer transitionen_US
dc.titleNew principle for aerodynamic heatingen_US
dc.identifier.doihttps://doi.org/10.1093/nsr/nwy035-
dc.typeArticleen_US
Appears in Collections:Eng - Journal articles (DHET subsidised)
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