Thermal modelling for the sustained hypersonic flight experiment
This paper details the development, validation and use of a thermal model created for the UK Ministry of Defence funded Sustained Hypersonic Flight Experiment (SHyFE). This compact ramjet will operate at Mach 4 to 6 leading to very high air flow stagnation temperatures. The thermal management system...
| Main Authors: | , |
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| Format: | Journal article |
| Language: | English |
| Published: |
2006
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