German Aerospace Center (DLR)
Published June 27, 2025 | Version v1
Dataset Open

Large Eddy Simulation of a Low-Pressure Turbine Cascade with Turbulent End Wall Boundary Layers - Supplemental Data

Authors/Creators

  • 1. German Aerospace Center (DLR)
  • 2. ROR icon Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
  • 3. MTU Aero Engines AG

Description

This provides supplemental data to Morsbach et al., Large Eddy Simulation of a Low-Pressure Turbine Cascade with Turbulent End Wall Boundary Layers, in Flow, Turbulence and Combustion (2024), https://doi.org/10.1007/s10494-023-00502-6.

The dataset contains

  • MTU-T161 geometry
  • boundary conditions for Reynolds number of 90000 and Mach number of 0.6
  • LES results
  • RANS results

as shown in the paper.

For a description of the files in the archive, see README.md. Code showing how to interpret the data files is given in plots.ipynb.

For more details, please refer to the paper.

Files

MTU-T161_LES_data_Morsbach2024_FTaC.zip

Files (16.2 MB)

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Additional details

Related works

Is supplement to
Journal article: 10.1007/s10494-023-00502-6 (DOI)