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...
第一著者: | Amend, JE |
---|---|
その他の著者: | Povey, T |
フォーマット: | 学位論文 |
言語: | English |
出版事項: |
2024
|
主題: |
類似資料
-
Development and aerothermal investigation of integrated combustor vane concept
著者:: Jacobi, S
出版事項: (2016) -
Non-Uniform Turbulence Modeling in Isolated Unsteady Diffuser Computational Models for a Vaned Centrifugal Compressor
著者:: Benjamin L. Holtmann, 等
出版事項: (2024-11-01) -
Development of a high-order implicit Discontinuous Galerkin method on unstructured meshes for turbomachinery flow
著者:: Min, Y
出版事項: (2018) -
QUALITATIVE COMPARISON OF 2D AND 3D COMPUTATION OF FLOW FIELD IN THE CONE SHAPED TURBINE NOZZLE
著者:: ROMUALD PUZYREWSKI, 等
出版事項: (2000-04-01) -
Lean-burn combustor simulator for an engine-component test facility: an experimental and computational study
著者:: Amend, J, 等
出版事項: (2023)