Design of heated flow wind tunnel facility for testing small size ramjet engine combustors
This report documents the research studies on the design of a 'high speed heated flow wind tunnel facility', to test a 'Trapped Vortex Concept' (TVC) combustor of a ramjet engine, designed for the DSO National Laboratories, Singapore. The ramjet is to operate at flight s...
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| Format: | Thesis |
| Language: | English |
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2015
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| Online Access: | http://hdl.handle.net/10356/65089 |