Please use this identifier to cite or link to this item: https://doi.org/10.1016/j.cja.2020.06.023
DC FieldValue
dc.titleAnalytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows
dc.contributor.authorHE, Z.
dc.contributor.authorJIANG, Z.
dc.contributor.authorZHANG, H.
dc.contributor.authorCHEN, W.
dc.date.accessioned2021-08-16T02:22:04Z
dc.date.available2021-08-16T02:22:04Z
dc.date.issued2020
dc.identifier.citationHE, Z., JIANG, Z., ZHANG, H., CHEN, W. (2020). Analytical method of nonlinear coupled constitutive relations for rarefied non-equilibrium flows. Chinese Journal of Aeronautics. ScholarBank@NUS Repository. https://doi.org/10.1016/j.cja.2020.06.023
dc.identifier.issn10009361
dc.identifier.urihttps://scholarbank.nus.edu.sg/handle/10635/196961
dc.description.abstractIt is well known that Navier-Stokes equations are not valid for those high-Knudsen and high-Mach flows, in which the local thermodynamically non-equilibrium effects are dominant. To extend the non-equilibrium describing the ability of macroscopic equations, Nonlinear Coupled Constitutive Relation (NCCR) model was developed from Eu's generalized hydrodynamic equations to substitute linear Newton's law of viscosity and Fourier's law of heat conduction in conservation laws. In the NCCR model, how to solve the decomposed constitutive equations with reasonable computational cost is a key ingredient of this scheme. In this paper, an analytic method is proposed firstly. Compared to the iterative procedure in the conventional NCCR model, the analytic method not only obtains exact roots of the decomposed constitutive polynomials, but also preserves the nonlinear constitutive relations in the original framework of NCCR methods. Numerical tests to assess the efficiency and accuracy of the proposed method are conducted for argon shock structures, Couette flows, two-dimensional hypersonic flows over a cylinder and three-dimensional supersonic flows over a three-dimensional sphere. These superior advantages of the current method are expected to render itself a powerful tool for simulating the hypersonic rarefied flows and microscale flows of high Knudsen number for engineering applications. © 2020 Chinese Society of Aeronautics and Astronautics
dc.publisherChinese Journal of Aeronautics
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.sourceScopus OA2020
dc.subjectKnudsen number
dc.subjectMicroscale flow
dc.subjectNon-equilibrium
dc.subjectNonlinear constitutive relations
dc.subjectRarefied gas
dc.typeArticle
dc.contributor.departmentMECHANICAL ENGINEERING
dc.description.doi10.1016/j.cja.2020.06.023
dc.description.sourcetitleChinese Journal of Aeronautics
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