A time-spectral approximate Jacobian based linearized compressible Navier-Stokes solver for high-speed boundary-layer receptivity and stability
•New method based on time-spectral approach to accurately predict the stability and receptivity of flows in complex geometries.•Higher-order spatial discretization of governing equations in disturbance flow formulation.•Pseudo-time marching for obtaining rapid solution of implicit time-spectral syst...
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Veröffentlicht in: | Journal of computational physics 2020-03, Vol.405, p.108978, Article 108978 |
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Format: | Artikel |
Sprache: | eng |
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Zusammenfassung: | •New method based on time-spectral approach to accurately predict the stability and receptivity of flows in complex geometries.•Higher-order spatial discretization of governing equations in disturbance flow formulation.•Pseudo-time marching for obtaining rapid solution of implicit time-spectral system.•2-D, 3-D, and axisymmetric solvers on generalized curvilinear mesh.•Validation of methods for a wide range of stability problems and receptivity test case.
A numerical method for conducting linear receptivity and stability investigations of high-speed wall-bounded flows based on the linearized compressible Navier-Stokes equations is presented. The current approach is directly applicable for stability investigations of arbitrarily complex geometries. The left-hand-side operator for the linear system of equations is obtained by computing numerical right-hand-side Jacobians while the right-hand-side is build from exact flux Jacobians. Utilizing the numerical right-hand-side Jacobian approach avoids lengthy, error prone derivation of the stability equations in the context of generalized curvilinear coordinates. The governing equations are solved using either time-stepping or time-spectral discretizations. Three different time-spectral approaches, i.e., direct inversion, unfactored and factored schemes, are presented and their numerical characteristics for the solution of the linearized Navier-Stokes equations for linear receptivity and stability analysis for large-scale transition problems are explored. Linear receptivity and stability calculation results are provided for different solver options. Performance comparison of the three schemes are presented for a wide range of test cases: An incompressible cross-flow for a swept flat plate boundary layer, a supersonic shock-boundary-layer interaction, hypersonic boundary layers on a flat plate and a flared cone, and, finally, for the receptivity of a hypersonic boundary layer for a right sharp cone. |
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ISSN: | 0021-9991 1090-2716 |
DOI: | 10.1016/j.jcp.2019.108978 |