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Leading-edge vortex development on a pitching flat plate with multiple leading edge geometries
Experimental Thermal and Fluid Science, 2018Abstract This article investigates the dynamic stall of a pitching flat plate in order to facilitate lift control in applications such as flapping wings and micro-aerial vehicles. Constant-pitch-rate rotation, similar to ramp-and-hold, of a flat plate was investigated in an open-jet wind tunnel using embedded surface pressure sensors to assess vortex
Leknys, R. +3 more
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Vortex separation above delta leading edges.
Journal of Aircraft, 1967and that the jet flow would attach at the inlet lip. The inspections of Fig. 4 shows that the round lip, created by the jet flow, extended well inside the inlet lip and restricted the inlet flow area. Thus, the pressure recovery improvements that might have been realized as the result of rounding the lip were offset by higher pressure losses associated
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Instabilities in Leading-Edge Vortex Development
5th Applied Aerodynamics Conference, 1987G.A. REYNOLDS, A.A. ABTAHI
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An experimental investigation of the entrainment into a leading-edge vortex
1981Aerospace ...
Verhaagen, N.G. (author) +1 more
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Slender Wings with Leading Edge Vortex-Separation
1982The demands of high speed performance and maneuverability on modern transport- and fighter-aircraft require slender wings, whose leading edge vortex flows result in increased lift at high angle-of-attack. Beginning with the experimental and theoretical development and the history of application the article will discuss the application of panel- and ...
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The entrainment effect of a leading-edge vortex
18th Fluid Dynamics and Plasmadynamics and Lasers Conference, 1985N. VERHAAGEN, A. KRUISBRINK
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Effects of leading-edge separation on the vortex-induced vibration of an elongated bluff body
Journal of Wind Engineering and Industrial Aerodynamics, 2021Guiyue Duan +2 more
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