32nd AIAA Fluid Dynamics Conference and Exhibit 2002
DOI: 10.2514/6.2002-3111
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Validation of the Unstructured DLR-TAU-Code for Hypersonic Flows

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Cited by 107 publications
(30 citation statements)
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“…This solver named rhoCentralFoam uses the central-upwind interpolation schemes of Kurganov and Tadmor [37]. It has been tested and assessed, and has been shown to produce similar results to those given by the MISTRAL flow solver [38] and the TAU code from the German Aerospace Center (DLR) [39] for the study of a non-reacting hypersonic flow past a hollow cylinder in the continuum regime [40]. Basic chemistry features have first been added to rhoCentralFoam by taking advantage of another OpenFOAM solver, reactingFoam, that covers subsonic combustion.…”
Section: Implementation In Openfoam 230mentioning
confidence: 97%
“…This solver named rhoCentralFoam uses the central-upwind interpolation schemes of Kurganov and Tadmor [37]. It has been tested and assessed, and has been shown to produce similar results to those given by the MISTRAL flow solver [38] and the TAU code from the German Aerospace Center (DLR) [39] for the study of a non-reacting hypersonic flow past a hollow cylinder in the continuum regime [40]. Basic chemistry features have first been added to rhoCentralFoam by taking advantage of another OpenFOAM solver, reactingFoam, that covers subsonic combustion.…”
Section: Implementation In Openfoam 230mentioning
confidence: 97%
“…The CFD computations for this study are performed by the hybrid structured/unstructured DLR Navier-Stokes Solver TAU [14]. The DLR-TAU-code is a second-order finite-volume flow solver for the Euler and Navier-Stokes equations in the integral form.…”
Section: Cfd-solver Taumentioning
confidence: 99%
“…The computational §uid dynamics (CFD) solutions are achieved with the unstructured DLR TAU-Code that has been validated in the past for di¨erent con¦gurations at super-and hypersonic §ow conditions [6], including extensive studies of wall jet injection [7,8] and combustion [9]. The time-accurate three-dimensional NavierStokes equations are marched for steady or unsteady conditions by an explicit three-stage Runge-Kutta scheme or an implicit LowerUpper Symmetric GaussSeidel (LUSGS) scheme.…”
Section: Numerical Modelingmentioning
confidence: 99%