Numerical Investigations of Transition in Hypersonic Flows over Circular Cones
This thesis focuses on secondary instability mechanisms of high-speed boundary layers over cones with a circular cross section. Hypersonic transition investigations at Mach 8 are performed using Direct Numerical Simulations (DNS). At wind-tunnel conditions, these simulations allow for comparison wit...
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| Language: | EN |
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The University of Arizona.
2008
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| Online Access: | http://hdl.handle.net/10150/196123 |