DANTEC DYNAMICS GmbH;LAVISION;MIT s.r.o.;TSI GmbH11th International Conference on Experimental Fluid Mechanics, EFM 2016 --15 November 2016 through 18 November 2016 -- --Present investigation focuses on unsteady flow structures in end-view planes at the trailing edge of delta wing, X/C=1.0, where consequences of vortex bursting and stall phenomena vary according to angles of attack over the range of 25° < ? <35° and yaw angles, ß over the range of 0° < ß < 20°. Basic features of counter rotating vortices in end-view planes of delta win with 70° sweep angle, ß are examined both qualitatively and quantitatively using Rhodamine dye and the PIV system. In the light of present experiments it is seen that with increasing yaw angle, ß symmetrical...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
Present investigation focuses on unsteady flow structures in end-view planes at the trailing edge of...
In the present experimental study, effects of yaw angle, ß on the flow structure at high angles of a...
DANTEC DYNAMICS GmbH;LAVISION;MIT s.r.o.;TSI GmbH12th International Conference on Experimental Fluid...
The dye injection and hydrogen bubble visualization techniques are used to investigate the dual-vort...
In the present investigation, flow structures over a slender delta wing with a 70° sweep angle, at a...
Aircraft that maneuver through large angles of attack will experience large regions of flow separati...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
The velocity eld near the apex region of moderately swept delta wings was measured in a water tunne...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
The flow structure on the upper side of a delta wing is extremely complex. At moderate angle of atta...
The velocity field near the apex region of moderately swept delta wings was measured in a water tunn...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
Present investigation focuses on unsteady flow structures in end-view planes at the trailing edge of...
In the present experimental study, effects of yaw angle, ß on the flow structure at high angles of a...
DANTEC DYNAMICS GmbH;LAVISION;MIT s.r.o.;TSI GmbH12th International Conference on Experimental Fluid...
The dye injection and hydrogen bubble visualization techniques are used to investigate the dual-vort...
In the present investigation, flow structures over a slender delta wing with a 70° sweep angle, at a...
Aircraft that maneuver through large angles of attack will experience large regions of flow separati...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
The velocity eld near the apex region of moderately swept delta wings was measured in a water tunne...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
The flow structure on the upper side of a delta wing is extremely complex. At moderate angle of atta...
The velocity field near the apex region of moderately swept delta wings was measured in a water tunn...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
In the present investigation, a delta wing which has 70° sweep angle, Λ was oscillated on its midcor...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...