2021
DOI: 10.1016/j.camwa.2020.03.009
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Nektar++: Design and implementation of an implicit, spectral/hp element, compressible flow solver using a Jacobian-free Newton Krylov approach

Abstract: At high Reynolds numbers the use of explicit in time compressible flow simulations with spectral/hp element discretization can become significantly limited by time step. To alleviate this limitation we extend the capability of the spectral/hp element open-source software framework, Nektar++, to include an implicit discontinuous Galerkin compressible flow solver. The integration in time is carried out by a singly diagonally implicit Runge-Kutta method. The non-linear system arising from the implicit time integr… Show more

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Cited by 20 publications
(28 citation statements)
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“…The solution converges well, almost monotonically, for Λ = 20 • and 30 • and, interestingly and in contrast to the straight wing, spanwise-uniform flow is found at terminal convergence. At the lower sweep angles of Λ = 5 • and 10 • , convergence stalls, failing to reach the specified tolerance, and different methods, such as selective frequency damping (Åkervik et al 2006) or a stronger implicit Newton-Krylov solver (Yan et al 2021), should be explored in the future to find fully converged base flow in those cases. Close inspection of the corresponding non-converged flow fields suggests indecisiveness in either forming spanwise cellular structures as for sweep angle Λ = 0 • or convergence towards spanwise-uniform flow as for the two largest sweep angles investigated.…”
Section: Spanwise-uniform Base Flow On Straight and Swept Wingsmentioning
confidence: 99%
“…The solution converges well, almost monotonically, for Λ = 20 • and 30 • and, interestingly and in contrast to the straight wing, spanwise-uniform flow is found at terminal convergence. At the lower sweep angles of Λ = 5 • and 10 • , convergence stalls, failing to reach the specified tolerance, and different methods, such as selective frequency damping (Åkervik et al 2006) or a stronger implicit Newton-Krylov solver (Yan et al 2021), should be explored in the future to find fully converged base flow in those cases. Close inspection of the corresponding non-converged flow fields suggests indecisiveness in either forming spanwise cellular structures as for sweep angle Λ = 0 • or convergence towards spanwise-uniform flow as for the two largest sweep angles investigated.…”
Section: Spanwise-uniform Base Flow On Straight and Swept Wingsmentioning
confidence: 99%
“…In what follows we briefly outline the formulation of a compressible flow solver based on a discontinuous Galerkin (DG) spatial discretization [13], an implicit time integration via ESDIRK temporal discretization schemes [17] and a JFNK method [16]. Further details of the solver can be found in reference [29].…”
Section: Governing Equations and Numerical Methodsmentioning
confidence: 99%
“…where w is the quadrature weight, J is the grid metric Jacobian, represents a diagonal matrix, = T (wJ) is the mass matrix, j is the derivative matrix in the jth direction, the superscript represents the corresponding matrices or variables on element boundaries, ̂ n j is a symmetric flux from the SIPG method, is the mapping matrix between and , and is the interpolation matrix from quadrature points of an element to quadrature points of its element boundaries. Details of the spatial discretization can be found in reference [29].…”
Section: Spatial Discretizationmentioning
confidence: 99%
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