Characterization of a Transitional Hypersonic Boundary Layer in Wind Tunnel and Flight Conditions
Laminar turbulent transition is known for a long time as a critical phenomenon influencing the thermal load encountered by hypersonic vehicle during their planetary re-entry trajectory. Despite the efforts made by several research laboratories all over the world, the prediction of transition remains...
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| Format: | Others |
| Language: | en |
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Universite Libre de Bruxelles
2009
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| Online Access: | http://theses.ulb.ac.be/ETD-db/collection/available/ULBetd-01152009-093721/ |