Influence of blade row aerodynamics on pneumatic gas turbine instrumentation
Steady state, inter row measurements in multistage axial compressors are relevant to the current design process. The objective in obtaining such data is for evaluation of compressor blading as well as validation for the computer programmes used in compressor design. Multi-hole pressure probes are a...
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| Language: | en |
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Cranfield University
2017
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/11295 |