On the Evaluation of Common Design Metrics for the Optimization of Non-Axisymmetric Endwall Contours for a 1-stage Turbine Rotor
With the continued economic and socio-political pressure on aircraft manufacturers to produce more profitable and environmentally-friendly aircraft, the drive towards increasingly more efficient aircraft engines remains of prime importance to aircraft engine manufacturers. While the majority of axia...
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| Format: | Doctoral Thesis |
| Language: | English |
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University of Cape Town
2019
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| Online Access: | http://hdl.handle.net/11427/29399 |