Techniques to quantify internal heat transfer of current and future effusion-cooled combustor walls
A requirement in the design and operation of gas turbines is to control the metal temperature of the combustor. One method by which this can be achieved is by passing compressor delivery air through arrays of cylindrical, angled effusion holes located in the combustor walls. However, recent advances...
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| Format: | Default Thesis |
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2020
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| Online Access: | https://dx.doi.org/10.26174/thesis.lboro.11955006.v1 |
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