Transitional shock wave/boundary-layer interaction unsteadiness on a cone-flare in hypersonic flow
<p>The causes of unsteadiness in hypersonic, axisymmetric, and transitional shock wave/boundary-layer interactions (SWBLIs) are investigated experimentally using a cone-flare model in the Oxford High Density Tunnel (HDT). The motivation of this research was to provide accurate measurements of...
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| Format: | Thesis |
| Language: | English |
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2023
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