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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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An experimental investigation of the entrainment into a leading-edge vortex
1981Aerospace ...
Verhaagen, N.G. (author) +1 more
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Instabilities in Leading-Edge Vortex Development
5th Applied Aerodynamics Conference, 1987G.A. REYNOLDS, A.A. ABTAHI
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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, 2021Li Hui, Shujin Laima
exaly
Turbulence modelling for leading-edge vortex flows
40th AIAA Aerospace Sciences Meeting & Exhibit, 2002H. Dol, J. Kok, B. Oskam
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