6th AIAA Theoretical Fluid Mechanics Conference 2011
DOI: 10.2514/6.2011-3753
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Coupling time-stepping numerical methods and standard aerodynamics codes for instabilitiy analysis of flows in complex geometries

Abstract: The development of a global instability analysis code coupling a time-stepping approach, as applied to the solution of BiGlobal and TriGlobal instability analysis 1, 2 and finite-volume-based spatial discretization, as used in standard aerodynamics codes is presented. The key advantage of the time-stepping method over matrix-formulation approaches is that the former provides a solution to the computer-storage issues associated with the latter methodology. To-date both approaches are successfully in use to anal… Show more

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Cited by 7 publications
(3 citation statements)
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“…35 In a different vein, application of Jacobian-Free Newton-Krylov methods to standard aerodynamic codes with the aim to study compressible flow instability over objects of arbitrary shape has commenced. 120 Details may respectively be found in the related contributions to this Conference.…”
Section: Discussionmentioning
confidence: 99%
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“…35 In a different vein, application of Jacobian-Free Newton-Krylov methods to standard aerodynamic codes with the aim to study compressible flow instability over objects of arbitrary shape has commenced. 120 Details may respectively be found in the related contributions to this Conference.…”
Section: Discussionmentioning
confidence: 99%
“…Although this situation is slowly changing in recent literature, 22,[117][118][119] global instability analysis is yet to penetrate into the world of classic CFD schemes, the latter typically being based on variants of low-order finite-volume methods. Gómez et al 120 present a Jacobian-Free Newton-Krylov based time-stepping algorithm of the class introduced into global instability analysis by Eriksson and Rizzi 121 and successfully employed to analyze BiGlobal 81,122 and TriGlobal 8 EVPs combined with a standard finite-volume solver for compressible flow capable of addressing compressible flows over complex geometries. Validation results, one of which is shown in figure 2, have been obtained by reference to the classic lid-driven cavity flow at low Reynolds numbers, as well as flow over a stalled airfoil; details may be found in Ref.…”
Section: Iva Time-stepping With Low-order Finite-volume Methodsmentioning
confidence: 99%
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