Dendritic cooling for nozzle guide vanes
<p>This thesis describes the development and characterisation of an entirely new form of gas turbine cooling scheme, in which passages repeatedly branch within the wall of the cooled component. This type of cooling is known as dendritic cooling. Such geometries offer particular performance imp...
| المؤلف الرئيسي: | |
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| مؤلفون آخرون: | |
| التنسيق: | أطروحة |
| اللغة: | English |
| منشور في: |
2011
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| الموضوعات: |