Shock wave turbulent boundary layer interaction over a protrusion
This research attempts to investigate an important and common phenomenon in aerodynamics called shock interaction in a turbulent flow’s boundary layer. Due to advancements in current computational units, more complex geometries could be simulated with providing more accurate results. The tools used...
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| Format: | Others |
| Language: | en_US |
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Wichita State University
2011
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| Online Access: | http://hdl.handle.net/10057/3942 |