Film cooling of gas turbine blades
An experimental apparatus was designed and built to study the film cooling effectiveness from a single row of holes at various angles and hole spacings, using a foreign gas technique. Mixtures of Freon 12 and air were injected into an air mainstream to give a range of density ratios encompassing the...
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| Format: | Thesis (University of Nottingham only) |
| Language: | English |
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1976
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| Online Access: | https://eprints.nottingham.ac.uk/13600/ |