Experimental investigation of vortex flaps on thick delta wings

[1]  W. E. Schoonover,et al.  Wind-tunnel investigation of vortex flaps on a highly swept interceptor configuration , 1982 .

[2]  Dhanvada M. Rao,et al.  Low-speed aerodynamics of apex fences on a tailless delta configuration , 1986 .

[3]  P. L. Coe,et al.  Effects of wing leading-edge deflection on the low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration , 1978 .

[4]  L. P. Yip,et al.  Effects of vortex flaps on the low-speed aerodynamic characteristics of an arrow wing , 1981 .

[5]  D. M. Rao,et al.  An investigation of the tabbed vortex flap , 1984 .

[6]  Dhanvada M Rao Vortical Flow Management for Improved Configuration Aerodynamics - Recent Experiences , 1983 .

[7]  E. Polhamus Predictions of vortex-lift characteristics based on a leading-edge suction analogy. , 1971 .

[8]  D. M. Rao,et al.  An exploratory study of area-efficient vortex flap concepts , 1983 .

[9]  J. Marchman The aerodynamics of inverted leading edge flaps on delta wings , 1981 .

[10]  D. M. Rao Upper Vortex Flap - A versatile surface for highly swept wings , 1982 .

[11]  D. Tavella,et al.  Analysis of a Delta Wing with Leading-Edge Flaps , 1987 .

[12]  Dhanvada M. Rao,et al.  Investigation of Delta Wing Leading-Edge Devices , 1981 .

[13]  J. F. Campbell,et al.  Vortex flaps - Advanced control devices for supercruise fighters , 1984 .

[14]  M. S. Chandrasekhara,et al.  A Study of Dynamic Stall Using Real Time Interferometry , 1994 .

[15]  P. L. Coe,et al.  Effects of wing leading-edge deflection on low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration. [wind tunnel tests] , 1979 .

[16]  Veer N. Vatsa,et al.  Navier-Stokes solutions for transonic flow over a wing mounted in a tunnel , 1988 .

[17]  P. Bradshaw,et al.  Turbulent Flow Measurements in an Idealized Wing/Body Junction , 1981 .

[18]  L. Roberts,et al.  Theoretical studies on flapped delta wings , 1988 .

[19]  J. F. Marchman Effectiveness of leading-edge vortex flaps on 60 and 75 degree delta wings , 1981 .