2016Unpublished venueRequires access

Analysis and Control of Partly-Developed Leading-Edge Vortices

Andreas Hövelmann

Open publisher page 6 citations

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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What this paper is about

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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Available 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.

Key concepts: Vortex, Leading edge, Enhanced Data Rates for GSM Evolution, Aerodynamics, Flow (mathematics), Mechanics, Wind tunnel, Wing

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