Diamond, Cropped, Delta, and Double-Delta Wing Vortex Breakdown During Dynamic Pitching

A series of experiments were conducted on the effect of different delta wing shapes on vortex breakdown under dynamic pitching conditions.

[1]  S. M. Batill,et al.  Vortex Dynamics on a Pitching Delta Wing , 1990 .

[2]  Ismet Gursul,et al.  Effect of shear-layer control on leading-edge vortices , 1996 .

[3]  J. F. Marchman lll Aerodynamics of Inverted Leading-Edge Flaps on Delta Wings , 1981 .

[4]  D. Degani,et al.  Experimental study of controlled tip disturbance effect on flow asymmetry , 1992 .

[5]  J. Steger Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries , 1978 .

[6]  D. Degani,et al.  Effect of geometrical disturbance on vortex asymmetry , 1991 .

[7]  Donald Rockwell,et al.  Transient response of leading-edge vortices to localized suction , 1990 .

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

[9]  N. J. Wood,et al.  Control of Vortical Lift on Delta Wings by Tangential Leading-Edge Blowing , 1988 .

[10]  Yuval Levy,et al.  ASYMMETRIC TURBULENT VORTICAL FLOWS OVER SLENDER BODIES , 1992 .

[11]  Robert C. Nelson,et al.  Double-delta-wing aerodynamics for pitching motions with and without sideslip , 1995 .

[12]  T. Maxworthy,et al.  GENERATION AND CONTROL OF SEPARATED VORTICES OVER A DELTA WING BY MEANS OF LEADING EDGE FLAPS , 1989 .

[14]  W. H. Wentz,et al.  Vortex breakdown on slender sharp-edged wings , 1969 .

[15]  Chih-Ming Ho,et al.  Lift Force of Delta Wings , 1990 .

[16]  J. A. Lawford Low-speed wind tunnel experiments on a series of sharp-edged delta wings: Part II. Surface flow patterns and boundary layer transition measurements , 1964 .

[17]  D. Degani,et al.  Numerical investigation of the origin of vortex asymmetry of flows over bodies at large angle of attack , 1990 .

[18]  Yuval Levy,et al.  Systematic study of the correlation between geometrical disturbances and flow asymmetries , 1996 .

[19]  R. F. Warming,et al.  An Implicit Factored Scheme for the Compressible Navier-Stokes Equations , 1977 .

[20]  D. Degani,et al.  Asymmetric Vortices on a Slender Body of Revolution , 1991 .

[21]  Gregory M. Gatlin,et al.  Low-speed longitudinal aerodynamic characteristics through poststall for 21 novel planform shapes , 1995 .

[22]  Roy Y. Myose,et al.  The effect of a 70 deg swept canard on the leading-edge vortices of a 70 deg swept delta wing during dynamic pitching , 1997 .

[23]  M. Salomon,et al.  Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowing , 1986 .

[24]  I Gursul,et al.  Control of vortex breakdown with leading-edge devices , 1995 .

[25]  P. J. Lamont,et al.  AIAA 80-1556R Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation , 2022 .

[26]  D. Degani,et al.  Effect of upstream disturbance on flow asymmetry , 1992 .

[27]  Brenda E. Gile,et al.  Effects of Blowing on Delta Wing Vortices During Dynamic Pitching , 1993 .

[28]  Lewis B. Schiff,et al.  Computation of turbulent supersonic flows around pointed bodies having crossflow separation , 1986 .

[29]  Gary E. Erickson,et al.  Water-Tunnel Studies of Leading-Edge Vortices , 1982 .

[30]  Lewis B. Schiff,et al.  NUMERICAL SIMULATION OF THE EFFECT OF SPATIAL DISTURBANCES ON VORTEX ASYMMETRY , 1989 .