An experimental and numerical investigation of the effect of aero gas turbine test facility aspect ratio on thrust measurement.
This work describes the outcome of research program investigating thrust measurements in enclosed test facility for modern aero gas turbine engines. Literature work, experimental work and a description of Computational fluid dynamics simulation system have been developed to improve the accuracy of t...
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| Language: | en |
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Cranfield University
2012
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/7224 |