Unsteady aerodynamics of nonslender delta wings
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[1] E. Vardaki. Aerodynamics of nonslender delta wings , 2006 .
[2] Raymond E. Gordnier,et al. Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing , 2005 .
[3] Ismet Gursul,et al. Review of Unsteady Vortex Flows over Slender Delta Wings , 2005 .
[4] I. Gursul,et al. Passive Flow Control over Flexible Non-Slender Delta Wings , 2005 .
[5] I. Gursul,et al. Physical mechanisms of lift enhancement for flexible delta wings , 2005 .
[6] M. Elkhoury,et al. Visualized vortices on unmanned combat air vehicle planform: Effect of Reynolds number , 2004 .
[7] Ismet Gursul,et al. Buffeting Flows over a Low-Sweep Delta Wing , 2004 .
[8] I. Gursul. Recent developments in delta wing aerodynamics , 2004, The Aeronautical Journal (1968).
[9] I. Gursul,et al. Vortex flows on a rolling nonslender delta wing , 2004 .
[10] Miguel R. Visbal,et al. Computation of the aeroelastic response of a flexible delta wing at high angles of attack , 2004 .
[11] Earl H. Dowell,et al. Modeling the LCO of a Delta Wing Using a High , 2004 .
[12] Donald Rockwell,et al. Flow Structure on a Delta Wing of Low Sweep Angle , 2004 .
[13] I. Gursul,et al. Unsteady vortex flows and buffeting of a low sweep delta wing , 2004 .
[14] Youssef Mébarki,et al. Experimental and Numerical Studies of Geometry Effects on UCAV's Aerodynamics , 2004 .
[15] Ismet Gursul,et al. Vortex flows on UAVs: Issues and challenges , 2002, The Aeronautical Journal (1968).
[16] Metin Yavuz,et al. Near-Surface Topology and Flow Structure on a Delta Wing with Low Sweep Angle , 2003 .
[17] Wei Shyy,et al. Membrane wing aerodynamics for micro air vehicles , 2003 .
[18] Ismet Gursul,et al. An Investigation of Vortex Flows over Low Sweep Delta Wings , 2003 .
[19] Miguel R. Visbal,et al. On the Structure of the Shear Layer Emanating from a Swept Leading Edge at Angle of Attack , 2003 .
[20] Earl H. Dowell,et al. Modeling Aerodynamic Nonlinearities for Two Aeroelastic Configurations: Delta Wing and Flapping Flag , 2003 .
[21] Lance W. Traub,et al. Extending Slender Wing Theory to Not So Slender Wings , 2003 .
[22] Michael V. Ol,et al. An Experimental Investigation of Leading Edge Vortices and Passage to Stall of Nonslender Delta Wings , 2003 .
[23] Earl H. Dowell,et al. A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model , 2003 .
[24] Richard Butler,et al. Aeroelastic Response of a Flexible Delta Wing Due to Unsteady Vortex Flows , 2003 .
[25] Miguel R. Visbal,et al. Higher-Order Compact Difference Scheme Applied to Low Sweep Delta Wing Flow , 2003 .
[26] L. Ericsson,et al. Analysis of Self-Induced Roll Oscillations of a 45-Degree Delta Wing , 2003 .
[27] Russell M. Cummings,et al. Numerical Predictions and Wind Tunnel Experiment for a Pitching Unmanned Combat Air Vehicle , 2003 .
[28] Michael V. Ol,et al. Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number , 2003 .
[29] I. Gursul,et al. Unsteady Aerodynamics of Low Aspect Ratio Wings at Low Reynolds Numbers , 2003 .
[30] S. Siegel,et al. PARTIAL LEADING EDGE FORCING OF A DELTA WING AT HIGH ANGLES OF ATTACK , 2002 .
[31] Avi Seifert,et al. Active flow control of a delta wing at high incidence using segmented piezoelectric actuators , 2002 .
[32] I. Gursul,et al. Vortex Flows over Fixed-Wing Micro Air Vehicles , 2002 .
[33] D. W. Bryer. The Bursting of Leading-Edge Vortices Some Observations and Discussion of the Phenomenon , 2002 .
[34] Lars E. Ericsson,et al. Wing Rock of Nonslender Delta Wings , 2001 .
[35] M. Ol,et al. The passage toward stall of nonslender delta wings at low Reynolds number , 2001 .
[36] Thomas McLaughlin,et al. PIV measurements on a delta wing with periodic blowing and suction , 2001 .
[37] Raymond E. Gordnier,et al. Numerical Simulation of Limit-cycle Oscillations of a Cropped Delta Wing Using the Full Navier-Stokes Equations , 2001 .
[38] Thomas J. Mueller,et al. Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers , 2001 .
[39] Earl H. Dowell,et al. Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing , 2001 .
[40] Thomas J. Mueller,et al. Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Wings , 2000 .
[41] Takashi Matsuno,et al. THE EFFECT OF LEADING-EDGE PROFILE ON SELF-INDUCED OSCILLATION OF 45-DEGREE DELTA WINGS , 2000 .
[42] N. Wood,et al. Aerodynamic characteristics of lambda wings , 2000, The Aeronautical Journal (1968).
[43] Takashi Matsuno,et al. Self-induced roll oscillation of 45-degree delta wings , 2000 .
[44] M. Woods. An investigation of buffet over low-observable planforms , 1999 .
[45] Ismet Gursul,et al. Experiments on the unsteady nature of vortex breakdown over delta wings , 1999 .
[46] Earl H. Dowell,et al. LIMIT CYCLE OSCILLATIONS OF DELTA WING MODELS IN LOW SUBSONIC FLOW , 1999 .
[47] Ismet Gursul,et al. Buffeting Flows over Delta Wings , 1999 .
[48] Takashi Matsuno,et al. UNSTEADY AERODYNAMICS OF ROLLING THICK DELTA WING WITH HIGH ASPECT RATIO , 1998 .
[49] Ismet Gursul,et al. Unsteady nature of leading edge vortices , 1997 .
[50] Edward T. Schairer,et al. Measurements of Unsteady Aeroelastic Model Deformation by Stereo Photogrammetry , 1997 .
[51] J. Andreopoulos,et al. Instantaneous Three-Dimensional Vorticity Measurements in Vortical Flow over a Delta Wing , 1997 .
[52] Miguel Visbal,et al. Computed unsteady structure of spiral vortex breakdown on delta wings , 1996 .
[53] D. W. Moore,et al. Inviscid separated flow over a non-slender delta wing , 1995, Journal of Fluid Mechanics.
[54] Miguel R. Visbal,et al. Origin of computed unsteadiness in the shear layer of delta wings , 1995 .
[55] Donald Rockwell,et al. Flow structure on stalled delta wing subjected to small amplitude pitching oscillations , 1995 .
[56] W. H. Liu,et al. Flow developments above 50-deg sweep delta wings with different leading-edge profiles , 1995 .
[57] M. Visbal,et al. Instabilities in the shear layer of delta wings , 1995 .
[58] Raymond E. Gordiner. Computation of vortex breakdown on a rolling delta wing , 1995 .
[59] M. Visbal,et al. Computational and physical aspects of vortex breakdown on delta wings , 1995 .
[60] Andrew Arena,et al. Experimental Investigations on Limit Cycle Wing Rock of Slender Wings , 1994 .
[61] H. Kawazoe,et al. Static and total pressure distributions around a thick delta wing with rounded leading edge , 1994 .
[62] Ismet Gursul,et al. Unsteady flow phenomena over delta wings at high angle of attack , 1994 .
[63] Miguel R. Visbal,et al. Unsteady vortex structure over a delta wing , 1994 .
[64] J. Délery. Aspects of vortex breakdown , 1994 .
[65] Donald Rockwell,et al. Three-dimensional flow structure on delta wings at high angle-of-attack - Experimental concepts and issues , 1993 .
[66] Jerry E. Jenkins,et al. Body-axis rolling motion critical states of a 65-degree delta wing , 1993 .
[67] J. Délery. Physics of Vortical Flows , 1992 .
[68] E. Hanff,et al. Roll-induced cross-loads on a delta wing at high incidence , 1991 .
[69] Joseph Katz,et al. Survey of research on unsteady aerodynamic loading of delta wings , 1991 .
[70] Juan Lopez,et al. Axisymmetric vortex breakdown Part 2. Physical mechanisms , 1990, Journal of Fluid Mechanics.
[71] Chih-Ming Ho,et al. Lift Force of Delta Wings , 1990 .
[72] Mohammad Reza Soltani,et al. Measurements on an oscillating 70-deg delta wing in subsonic flow , 1990 .
[73] O. Rediniotis,et al. Periodic vortex shedding over delta wings , 1989 .
[74] Jerome T. Kegelman,et al. Effects of leading-edge shape and vortex burst on the flowfield of a70-degree-sweep delta-wing , 1989 .
[75] Robert V. Doggett,et al. Some low-speed flutter characteristics of simple low-aspect-ratio delta wing models , 1989 .
[76] R. Blackwelder,et al. Control of the discrete vortices from a delta wing , 1986 .
[77] Mohamed Gad-el-Hak,et al. The discrete vortices from a delta wing , 1985 .
[78] Jerome T. Kegelman,et al. Control of coherent structures in reattaching laminar and turbulent shear layers , 1985 .
[79] Gary E. Erickson,et al. Water-Tunnel Studies of Leading-Edge Vortices , 1982 .
[80] E. Polhamus. Predictions of vortex-lift characteristics based on a leading-edge suction analogy. , 1971 .
[81] E. Polhamus,et al. Predictions of vortex-lift characteristics based on a leading-edge suction analogy , 1969 .
[82] W. H. Wentz,et al. Vortex breakdown on slender sharp-edged wings , 1969 .
[83] M. V. Lowson,et al. Some Experiments with Vortex Breakdown , 1964, The Journal of the Royal Aeronautical Society.
[84] 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 .
[85] R. J. Vidal,et al. Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Speeds , 1955 .