Thermal effects of plume impingement on a hypersonic vehicle
The thermal effects of plume impingement on the uselage of a hypersonic vehicle were investigated using a plume generator mounted to a flat plate model in the Oxford High Density Tunnel at Mach 7. The model was instrumented with thin film heat transfer gauges, pressure transducers, Pressure Sensitiv...
| Päätekijät: | , , , , |
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| Aineistotyyppi: | Conference item |
| Kieli: | English |
| Julkaistu: |
Council of European Aerospace Societies
2022
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