A wing is described for aircraft of cropped, arrow-type planform with thin leading and side edges. The wing has a pivotable tip to alter the crop angle of the wing during flight. Increasing the crop angle causes the wing side edge to become a trailing edge which reduces the strength of the side edge vortex flow. Decreasing the crop angle causes opposite results, in particular the side edge is now a leading edge and can generate a leading edge vortex flow. The wing constitutes a roll control device for aircraft of the stated design particularly effective at higher angles of attack.
Vortex-Lift Roll-Control Device
1977
6 pages
Report
Keine Angabe
Englisch
Vortex-lift roll-control device
NTRS | 1979
|Vortex-Lift Roll-Control Device
NTIS | 1977
|Wake Evolution of High-Lift Configuration from Roll-Up to Vortex Decay
British Library Conference Proceedings | 2013
|