Effect of lean-burn combustor outlet flows on nozzle guide vane aerothermal performance: an experimental and computational study
<p>Regulatory pressures aimed at reducing NOx and particulate emissions from civil aviation have seen engine manufacturers gravitate towards lean-burn combustor architectures. Compared to their conventional <em>rich-burn</em> counterparts, lean-burn combustors generate significant...
Päätekijä: | Amend, JE |
---|---|
Muut tekijät: | Povey, T |
Aineistotyyppi: | Opinnäyte |
Kieli: | English |
Julkaistu: |
2024
|
Aiheet: |
Samankaltaisia teoksia
-
Development and aerothermal investigation of integrated combustor vane concept
Tekijä: Jacobi, S
Julkaistu: (2016) -
Non-Uniform Turbulence Modeling in Isolated Unsteady Diffuser Computational Models for a Vaned Centrifugal Compressor
Tekijä: Benjamin L. Holtmann, et al.
Julkaistu: (2024-11-01) -
Development of a high-order implicit Discontinuous Galerkin method on unstructured meshes for turbomachinery flow
Tekijä: Min, Y
Julkaistu: (2018) -
QUALITATIVE COMPARISON OF 2D AND 3D COMPUTATION OF FLOW FIELD IN THE CONE SHAPED TURBINE NOZZLE
Tekijä: ROMUALD PUZYREWSKI, et al.
Julkaistu: (2000-04-01) -
Lean-burn combustor simulator for an engine-component test facility: an experimental and computational study
Tekijä: Amend, J, et al.
Julkaistu: (2023)