Effect of transpiration cooling on boundary layer transition for hypersonic flight
<p>Superseding ablative cooling techniques with active thermal protection could benefit the development of hypersonic flight technology by improving resistance of vehicles to thermal loads, re-usability and shape stability. Transpiration cooling could ensure protection of areas that are most a...
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| Médium: | Diplomová práce |
| Jazyk: | English |
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2022
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