Experimental studies of hypersonic shock impingement on a transpiration-cooled flat plate
Hypersonic vehicle design requires mitigation of the high heat fluxes present in regions of shock-wave/boundary-layer interactions. A candidate technology that may be applied locally to these regions is transpiration cooling. In this work, experiments were conducted in the University of Oxford’s hig...
| Main Authors: | , , , |
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| 格式: | Journal article |
| 語言: | English |
| 出版: |
American Institute of Aeronautics and Astronautics
2023
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