Analysis and Control of Partly-Developed Leading-Edge Vortices
Andreas Hövelmann
Abstract
Andreas Hövelmann
Abstract
This doctoral thesis focuses on leading-edge vortex flow phenomena associated with two moderately-swept, low-aspect-ratio diamond wing configurations. Combined experimental and numerical investigations were undertaken at low-speed wind tunnel conditions. A consistent flow-physical description of the leading-edge vortex formation and progression due to rounded leading edges is provided. Also, spanwise-varying leading-edge contours are considered, and the effects on leading-edge vortex separations and aerodynamic characteristics are reviewed.
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This doctoral thesis focuses on leading-edge vortex flow phenomena associated with two moderately-swept, low-aspect-ratio diamond wing configurations. Combined experimental and numerical investigations were undertaken at low-speed wind tunnel conditions. A consistent flow-physical description of the leading-edge vortex formation and progression due to rounded leading edges is provided. Also, spanwise-varying leading-edge contours are considered, and the effects on leading-edge vortex separations and aerodynamic characteristics are reviewed.
Key concepts: Vortex, Leading edge, Enhanced Data Rates for GSM Evolution, Aerodynamics, Flow (mathematics), Mechanics, Wind tunnel, Wing