Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Silvia Reuss"'
A new low-dissipation low-dispersion second-order scheme is applied to scale-resolving flow simulations using compressible and incompressible unstructured finite volume solvers. In wall-resolved and wall-modeled large-eddy simulations of the plane ch
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::71c614f5665c502e294000411fd3ebf6
https://doi.org/10.2514/1.j054957
https://doi.org/10.2514/1.j054957
Autor:
Rolf Radespiel, Thorsten Lutz, Silvia Reuss, Katharina Wawrzinek, Tobias Knopp, Rainer Hain, Torsten Auerswald, David Hoppmann, Christoph Knigge, Ralf Heinrich, Daniela Gisele François, Jens Bange, Christian J. Kähler, Peter Scholz, Simon Klein, Axel Probst, Siegfried Raasch, Philip Kelleners, Simon Übelacker
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Numerical stall simulations are challenging in terms of physical models involved, overall computation effort, and the needed efforts for validation. The present paper describes coordinated, fundamental research into new simulation methodologies and t
Publikováno v:
International Journal for Numerical Methods in Fluids. 70:1558-1572
The Chimera technique for moving grids is used to take into account non-homogeneous unsteady onflow conditions in the simulation of aerodynamic flows. The method is applied to simulate the transport of a large-scale vortex by a mean velocity field ov
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319211268
We consider the numerical simulation of a generic lateral vortex, that is generated by a rapidly deflected NACA0021 airfoil. We use the SST k-\(\omega \) URANS approach and a hybrid RANS-LES method based on the SST model, where a zonal RANS-LES inter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9e1e054bc59b9f236fee958a37fd7e2d
https://doi.org/10.1007/978-3-319-21127-5_3
https://doi.org/10.1007/978-3-319-21127-5_3
Autor:
Axel Probst, Silvia Reuß
Publikováno v:
Progress in Hybrid RANS-LES Modelling ISBN: 9783319151403
The fully-developed channel flow at \(Re_\tau \approx 395\) is used to validate scale-resolving simulations with the unstructured compressible DLR-TAU code. In a sensitivity study based on wall-resolved LES a low-dissipative spatial scheme is derived
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::15d4f2463193f3ca75b3686df723be7e
https://elib.dlr.de/96152/
https://elib.dlr.de/96152/
A new low-dissipation low-dispersion 2nd-order scheme is applied to scale-resolving flow simulations using compressible and incompressible unstructured finite-volume solvers. In wall-resolved and wall-modeled LES computations of the channel flow t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b2b5a7b3d361c9e20a0bfb70ad6977f6
https://doi.org/10.2514/6.2015-0816
https://doi.org/10.2514/6.2015-0816
Publikováno v:
Progress in Hybrid RANS-LES Modelling ISBN: 9783319151403
Different sensors that provide a measure for the resolution of the LES content in hybrid RANS/LES computations are proposed and investigated. In an a-priori test on isotropic turbulence a suitable sensor is identified. Based on that sensor an automat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ddccf08eea274343644a8f4833233bfb
https://doi.org/10.1007/978-3-319-15141-0_7
https://doi.org/10.1007/978-3-319-15141-0_7
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319211268
In an effort to accurately compute nacelle stall processes, the research unit FOR1066 (Simulation of Wing and Nacelle Stall) has been working extensively on the development of advanced simulation methods. Due to the high dependency of the separation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f3d7a097f0f35c5975048adec262523a
https://elib.dlr.de/95283/
https://elib.dlr.de/95283/
Publikováno v:
Progress in Hybrid RANS-LES Modelling ISBN: 9783642318177
In this paper the Spalart-Allmaras based Delayed Detached Eddy Simulation (DDES [1]) and Improved Delayed Detached Eddy Simulation (IDDES [2]) are used to simulate the flow about an industrially relevant airfoil-configuration with deployed high-lift
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d2a1ee0601df074927277f88fa815fd7
https://elib.dlr.de/71919/
https://elib.dlr.de/71919/
Autor:
Thorsten Lutz, Peter Scholz, Daniela Gisele François, Tobias Knopp, Rolf Radespiel, Siegfried Raasch, Katharina Wawrzinek, Ralf Heinrich, Axel Probst, Simon Klein, Torsten Auerswald, Jens Bange, Silvia Reuß, David Hoppmann, Philip Kelleners, Christoph Knigge
Publikováno v:
Scopus-Elsevier
Simulation capabilities for low-speed aircraft stall prediction are important for determining the limits of safe aircraft operations during design processes. The simulations are extremely demanding in terms of physical models involved, overall comput
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bc169357321619bbba2efa3a0a13583c
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883591109&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84883591109&partnerID=MN8TOARS