Integrated design of compressor transition ducts with swirling flow and aerodynamic lifting struts
To meet future environmental and economic targets aero gas turbines will require the development of new core engine technologies, higher overall pressure ratios and improved efficiencies. In a multistage intermediate-pressure compressor an efficiency benefit may be gained by reducing reaction in the...
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| Format: | Default Thesis |
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2018
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| Online Access: | https://dx.doi.org/10.26174/thesis.lboro.8153471.v1 |
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