Numerical Investigation of Boundary-Layer Transition for Cones at Mach 3.5 and 6.0
Transition in high-speed boundary layers is investigated using direct numerical simulation (DNS). A compressible Navier-Stokes code that is specifically tailored towards accurate and efficient simulations of boundary layer stability and boundary layer transition was developed and thoroughly validat...
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| Language: | en |
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The University of Arizona.
2011
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| Online Access: | http://hdl.handle.net/10150/205419 |