Source Term-Based Synthetic Turbulence Generator Applied to Compressible DNS of the T106A Low-Pressure Turbine
Direct numerical simulations (DNSs) of the T106A low-pressure turbine were conducted for various turbulence intensities and length scales to investigate their effects on flow behaviour and transition. A source-term formulation of the synthetic eddy method (SEM) was implemented in the Nektar++ spectral/hp element framework to introduce anisotropic turbulence into the flow field. A single sponge layer was imposed, which covers the inflow and outflow regions just downstream and upstream of the inflow and outflow boundaries, respectively, to avoid acoustic wave reflections on the boundary conditions. Additionally, in the T106A model, mixed polynomial orders were utilized, as Nektar++ allows different polynomial orders for adjacent elements. A lower polynomial order was employed in the outflow region to further assist the sponge layer by coarsening the mesh and diffusing the turbulence near the outflow boundary. Thus, this study contributes to the development of a more robust and efficient model for high-fidelity simulations of turbine blades by enhancing stability and producing a more accurate flow field. The main findings are compared with experimental and DNS data, showing good agreement and providing new insights into the influence of turbulence length scales on flow separation, transition, wake behaviour, and loss profiles.
Authors
- João Anderson Isler (ORCID: https://orcid.org/0000-0003-1284-8140)
- Chris D. Cantwell (ORCID: https://orcid.org/0000-0002-2448-3540)
- Francesco Montomoli (ORCID: https://orcid.org/0000-0002-2241-3389)
- Guglielmo Vivarelli (ORCID: https://orcid.org/0000-0003-4731-3509)
- Spencer J. Sherwin (ORCID: https://orcid.org/0000-0001-7681-2820)
- Marcus Meyer (ORCID: https://orcid.org/0000-0003-4527-7815)
- Raúl Vázquez
- Yuri Frey
Institutions
- Rolls-Royce (Germany) (DE)
- Scuola Superiore Sant'Anna (IT)
- Imperial College London (GB)
- Rolls-Royce (United Kingdom) (GB)
Publication Details
- Journal
- International Journal of Turbomachinery Propulsion and Power
- Published
- 2025-07-04
- DOI
- https://doi.org/10.3390/ijtpp10030013
- Citations
- 1
- Primary Topic
- Combustion and flame dynamics
- Type
- article
- Field-Weighted Citation Impact
- 1.33