Wing Rock of Nonslender Delta Wings

That slender delta wings will experience wing rock is an established fact, and the responsible flow mechanism is well understood. However, the same flow mechanism could not cause wing rock of nonslender delta wings. Thus, the wing rock observed for a 45-deg delta wing must be generated by a different flow phenomenon. Experimental results for delta wings and airfoils are analyzed in order to define the flow mechanism driving the observed wing-rock motion

[1]  James H. Myatt,et al.  Body-axis rolling motion critical states of a 65-degree delta wing , 1993 .

[2]  L. E. Ericsson,et al.  Various sources of wing rock , 1990 .

[3]  Lars E. Ericsson Analysis of the effect of sideslip on delta wing roll trim characteristics , 1997 .

[4]  E. Hanff,et al.  Large-amplitude high-rate roll experiments on a delta and double delta wing , 1990 .

[5]  Lars E. Ericsson Partial-Span Leading-Edge Vortex Characteristics in High-Rate Oscillations in Pitch , 1997 .

[6]  Lars E. Ericsson,et al.  Effect of leading-edge geometry on delta wing unsteady aerodynamics , 1993 .

[7]  Lars E. Ericsson,et al.  Flow Physics of Critical States for Rolling Delta Wings , 1995 .

[8]  Eastman N. Jacobs,et al.  Airfoil section characteristics as affected by variations of the Reynolds number , 1939 .

[9]  Lars E. Ericsson,et al.  Unique High-Alpha Roll Dynamics of a Sharp-Edged 65-Deg Delta Wing , 1994 .

[10]  Lars E. Ericsson Wing rock analysis of slender delta wings - Review and extension , 1995 .

[11]  Jerry E. Jenkins,et al.  Body-axis rolling motion critical states of a 65-degree delta wing , 1993 .

[12]  Lars E. Ericsson Moving wall effect in relation to other dynamic stall flow mechanisms , 1994 .

[13]  Lars E. Ericsson,et al.  Further analysis of high-rate rolling experiments of a 65-deg delta wing , 1994 .

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

[15]  L. E. Ericsson,et al.  Rapid prediction of high-alpha unsteady aerodynamics of slender-wingaircraft , 1992 .

[16]  Lars E. Ericsson Effect of angle of attack on roll characteristics of 65-degree delta wing , 1997 .

[17]  Takashi Matsuno,et al.  UNSTEADY AERODYNAMICS OF ROLLING THICK DELTA WING WITH HIGH ASPECT RATIO , 1998 .

[18]  Donald Rockwell,et al.  Flow structure on stalled delta wing subjected to small amplitude pitching oscillations , 1995 .

[19]  E. Hanff,et al.  Prediction of leading-edge vortex breakdown on a delta wing oscillating in roll , 1992 .

[20]  Luat T. Nguyen,et al.  Use of the updated NASA Langley radio-controlled drop-model technique for high-alpha studies of the X-29A configuration , 1987 .