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...
Príomhchruthaitheoir: | Amend, JE |
---|---|
Rannpháirtithe: | Povey, T |
Formáid: | Tráchtas |
Teanga: | English |
Foilsithe / Cruthaithe: |
2024
|
Ábhair: |
Míreanna comhchosúla
Míreanna comhchosúla
-
Development and aerothermal investigation of integrated combustor vane concept
de réir: Jacobi, S
Foilsithe / Cruthaithe: (2016) -
Non-Uniform Turbulence Modeling in Isolated Unsteady Diffuser Computational Models for a Vaned Centrifugal Compressor
de réir: Benjamin L. Holtmann, et al.
Foilsithe / Cruthaithe: (2024-11-01) -
Development of a high-order implicit Discontinuous Galerkin method on unstructured meshes for turbomachinery flow
de réir: Min, Y
Foilsithe / Cruthaithe: (2018) -
QUALITATIVE COMPARISON OF 2D AND 3D COMPUTATION OF FLOW FIELD IN THE CONE SHAPED TURBINE NOZZLE
de réir: ROMUALD PUZYREWSKI, et al.
Foilsithe / Cruthaithe: (2000-04-01) -
Lean-burn combustor simulator for an engine-component test facility: an experimental and computational study
de réir: Amend, J, et al.
Foilsithe / Cruthaithe: (2023)