A delta wing is subjected to both static and dynamic variations of angle-of-attack; the vortices from the wing impinge upon a stationary plate. A technique of high-image-density particle image velocimetry is employed to compare the patterns of vortex development with and without the impingement plate. For the limiting case of static variations of angle-of-attack, the presence of the plate exerts a large influence on the onset of vortex breakdown. In contrast, dynamic (unsteady) variation of angle-of-attack yields changes of breakdown location that are generally similar for cases with and without the impingement plate. The detailed structure of the vortex breakdown-plate interaction is represented by patterns of instantaneous velocity and vo...
Wind-tunnel experiments were performed to study the complex flow mechanisms on a 70-deg. sharp leadi...
A series of flow visualization tests of a uniformly pitching, 60° sweep delta wing have been perform...
It has been demonstrated that leading edge vortices (LEVs) formed by airflow past an elevated delta ...
A delta wing is subjected to both static and dynamic variations of, angle-of-attack; the vortices fr...
A delta wing is subjected to small-amplitude perturbations over a range of periods, to simulate lead...
A delta wing is subjected to small-amplitude perturbations over a range of periods, to simulate lead...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
Flow past the leading edge of a delta wing oscillating about its mid-cord in a pitch plane with a re...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
Flow past the leading edge of a delta wing oscillating about its mid-cord in a pitch plane with a re...
Flow past the leading edge of a delta wing oscillating about its mid-cord in a pitch plane with a re...
The flow structure on the upper side of a delta wing is extremely complex. At moderate angle of atta...
Aircraft that maneuver through large angles of attack will experience large regions of flow separati...
Wind-tunnel experiments were performed to study the complex flow mechanisms on a 70-deg. sharp leadi...
Wind-tunnel experiments were performed to study the complex flow mechanisms on a 70-deg. sharp leadi...
A series of flow visualization tests of a uniformly pitching, 60° sweep delta wing have been perform...
It has been demonstrated that leading edge vortices (LEVs) formed by airflow past an elevated delta ...
A delta wing is subjected to both static and dynamic variations of, angle-of-attack; the vortices fr...
A delta wing is subjected to small-amplitude perturbations over a range of periods, to simulate lead...
A delta wing is subjected to small-amplitude perturbations over a range of periods, to simulate lead...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
Flow past the leading edge of a delta wing oscillating about its mid-cord in a pitch plane with a re...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
Flow past the leading edge of a delta wing oscillating about its mid-cord in a pitch plane with a re...
Flow past the leading edge of a delta wing oscillating about its mid-cord in a pitch plane with a re...
The flow structure on the upper side of a delta wing is extremely complex. At moderate angle of atta...
Aircraft that maneuver through large angles of attack will experience large regions of flow separati...
Wind-tunnel experiments were performed to study the complex flow mechanisms on a 70-deg. sharp leadi...
Wind-tunnel experiments were performed to study the complex flow mechanisms on a 70-deg. sharp leadi...
A series of flow visualization tests of a uniformly pitching, 60° sweep delta wing have been perform...
It has been demonstrated that leading edge vortices (LEVs) formed by airflow past an elevated delta ...