1999
DOI: 10.1007/978-3-663-10901-3_55
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On the Validation of the DLR-TAU Code

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Cited by 94 publications
(71 citation statements)
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“…The DLR TAU code [8] is used to compute the §ow¦elds by solving the RANS equations for compressible §ow [9]. The equations are discretited by a secondorder ¦nite volume approach on hexahedral grids.…”
Section: Numerical Settingsmentioning
confidence: 99%
“…The DLR TAU code [8] is used to compute the §ow¦elds by solving the RANS equations for compressible §ow [9]. The equations are discretited by a secondorder ¦nite volume approach on hexahedral grids.…”
Section: Numerical Settingsmentioning
confidence: 99%
“…The computation is continued so that the gust is propagated through the flow field. In the approach by Kelleners and Heinrich (2015) and Reimer et al (2015) using TAU (Schwamborn et al, 2006) to solve the compressible RANS equations, the gust is transported with the speed of sound. In their approach, as well as in the present paper, the computation has been run at least until the gust has entirely passed the geometry in question but can be continued as long as wished by the user.…”
Section: The Resolved-gust Approachmentioning
confidence: 99%
“…Kelleners and Heinrich (2015) and Reimer et al (2015) presented two approaches which are implemented in the URANS solver TAU (Schwamborn et al, 2006) to apply vertical gusts on airplanes: the velocitydisturbance approach and the resolved-gust approach. The velocity-disturbance approach adds the gust velocity to the surface of the investigated geometry.…”
Section: Introductionmentioning
confidence: 99%
“…6g); (e) symmetry plane of the computational grid with Chimera interpolation zones; (f ) cross section of the computational grid for αAD = 0 • ; and (g) longitudinal cut of the computational grid with interpolation zones TAU-code [29]. The §ow properties of the numerical simulation are: M = 2.2, Re = 296000, T 0 = 315 K, and u ∞ = 782.7 m/s.…”
Section: Numerical Approachmentioning
confidence: 99%