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...
| Main Authors: | , , , , |
|---|---|
| 格式: | Conference item |
| 语言: | English |
| 出版: |
Council of European Aerospace Societies
2022
|