Evolution of an Acoustic Disturbance to Transition in the Boundary Layer on an Airfoil
An experiment has been conducted to examine the generation and subsequent evolution of boundary-layer disturbances on a two-dimensional airfoil up through transition to turbulent flow. The experiment was conducted at the NASA Langley Research Center "2 ft by 3 ft Low Speed Wind Tunnel Facility....
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| Format: | Others |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/26603 http://scholar.lib.vt.edu/theses/available/etd-040299-143904/ |