Lift Augmentation on a Delta Wing via Leading Edge Fences and the Gurney Flap
暂无分享,去创建一个
[1] Joseph Katz,et al. Effect of 90 Degree Flap on the Aerodynamics of a Two-Element Airfoil , 1989 .
[2] J. Marchman. The aerodynamics of inverted leading edge flaps on delta wings , 1981 .
[3] Experimental analysis of vortex trapping techniques , 1991 .
[4] W. H. Wentz,et al. Vortex breakdown on slender sharp-edged wings , 1969 .
[5] Vernon J. Rossow,et al. Two-fence concept for efficient trapping of vortices on airfoils , 1992 .
[6] R. Liebeck. Design of Subsonic Airfoils for High Lift , 1976 .
[7] Russell M. Cummings,et al. Computational evaluation of an airfoil with a Gurney flap , 1992 .
[8] P. S. Srinivasan,et al. Vortex Breakdown Effects on the Low-speed Aerodynamic Characteristics of Slender Delta Wings in Symmetrical Flow , 1967, The Journal of the Royal Aeronautical Society.
[9] Odis C. Pendergraft,et al. A water tunnel study of Gurney flaps , 1988 .
[10] Vernon J. Rossow,et al. Aerodynamics of airfoils with vortex trapped by two spanwise fences , 1991 .
[11] Turgut Sarpkaya,et al. Vortex Breakdown in Swirling Conical Flows , 1971 .
[12] Turgut Sarpkaya,et al. Effect of the Adverse Pressure Gradient on Vortex Breakdown , 1974 .
[13] Cary Moskovitz,et al. Experimental investigation of apex fence flaps on delta wings , 1985 .
[14] V. Rossow. Lift enhancement by an externally trapped vortex , 1978 .