Optimising wing lift distribution to minimise wake vortex hazard

Aeronautical Journal

Volumn 106, Issue 1062, 2002, Pages 413-426

  Graham, W R ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; LIFT; OPTIMIZATION; VORTEX FLOW; WAKES; WINGS;

FLAP; INVISCID VORTEX METHOD; ROLLING MOMENT; WAKE VORTEX HAZARD; WING LIFT DISTRIBUTION;

TRANSPORT AIRCRAFT;

EID: 0036686629     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (19)

1. Aerial flight
2. Lift-generated vortex wakes of subsonic transport aircraft
3. Airplane trailing vortices
4. Panel discussion
5. Instability and transient growth for two trailing vortex pairs
6. Method for accelerating the destruction of aircraft wake vortices
7. Active-control system for breakup of airplane trailing vortices
8. Wake alleviation properties of triangular-flapped wings
9. Axial flow in trailing line vortices
10. An assessment of the 2D vortex method in aircraft wake simulation
11. Vortex methods for flow simulation
12. Computation of vortex sheet roll-up in the Trefftz plane
13. Experimental assessment of the extended Betz method for wake vortex prediction
14. Calculation of aircraft wake velocity profiles and comparison with experimental measurements
15. The structure and development of a wing-tip vortex
16. The structure and development of a counter-rotating wing-tip vortex pair
17. Flow structure produced by the interaction and merger of a pair of co-rotating wing-tip vortices
18. Vortex methods for separated flows