We present a solver for DNS of turbulent compressible flows over arbitrary shaped geometries. The code solves the compressible Navier-Stokes equations in a generalized curvilinear coordinates system, using high-order central finite-difference schemes combined with WENO reconstruction for shock-waves treatment. An innovative stabilization strategy for central schemes based on skew-symmetric-like splitting of convective derivatives is used. The code is oriented to modern HPC platforms thanks to MPI parallelization and the ability to run on GPU architectures. The robustness and accuracy of the present code is assessed both in the low-subsonic case and in the supersonic case. We show here the results of a turbulent curved channel flow and a turbulent supersonic compression ramp, which proved to be in excellent match with previous studies.

Development of a DNS solver for compressible flows in generalized curvilinear coordinates / Soldati, Giulio; Ceci, Alessandro; Pirozzoli, Sergio. - 37:(2023), pp. 222-225. (Intervento presentato al convegno Aeronautics and Astronautics - AIDAA XXVII International Congress tenutosi a Padova) [10.21741/9781644902813-48].

Development of a DNS solver for compressible flows in generalized curvilinear coordinates

Soldati, Giulio
Primo
;
Ceci, Alessandro
Secondo
;
Pirozzoli, Sergio
Ultimo
2023

Abstract

We present a solver for DNS of turbulent compressible flows over arbitrary shaped geometries. The code solves the compressible Navier-Stokes equations in a generalized curvilinear coordinates system, using high-order central finite-difference schemes combined with WENO reconstruction for shock-waves treatment. An innovative stabilization strategy for central schemes based on skew-symmetric-like splitting of convective derivatives is used. The code is oriented to modern HPC platforms thanks to MPI parallelization and the ability to run on GPU architectures. The robustness and accuracy of the present code is assessed both in the low-subsonic case and in the supersonic case. We show here the results of a turbulent curved channel flow and a turbulent supersonic compression ramp, which proved to be in excellent match with previous studies.
2023
Aeronautics and Astronautics - AIDAA XXVII International Congress
Generalized Curvilinear Coordinates; Shock-Wave/Boundary Layer Interaction; Turbulent Compression Ramp; Curved Channel Flow
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Development of a DNS solver for compressible flows in generalized curvilinear coordinates / Soldati, Giulio; Ceci, Alessandro; Pirozzoli, Sergio. - 37:(2023), pp. 222-225. (Intervento presentato al convegno Aeronautics and Astronautics - AIDAA XXVII International Congress tenutosi a Padova) [10.21741/9781644902813-48].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1703815
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