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...
المؤلف الرئيسي: | Amend, JE |
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مؤلفون آخرون: | Povey, T |
التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2024
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الموضوعات: |
مواد مشابهة
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Development and aerothermal investigation of integrated combustor vane concept
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Development of a high-order implicit Discontinuous Galerkin method on unstructured meshes for turbomachinery flow
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QUALITATIVE COMPARISON OF 2D AND 3D COMPUTATION OF FLOW FIELD IN THE CONE SHAPED TURBINE NOZZLE
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منشور في: (2000-04-01) -
Lean-burn combustor simulator for an engine-component test facility: an experimental and computational study
حسب: Amend, J, وآخرون
منشور في: (2023)