Trailing vortices from a wing with a notched lift distribution

AIAA Journal

Volumn 41, Issue 9, 2003, Pages 1835-1838

  Graham, W R ^a   Park, S W ^a   Nickels, T B ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; CAMERAS; COMPUTER SIMULATION; DATA ACQUISITION; LIFT; SOLID STATE LASERS; VELOCITY MEASUREMENT; VORTEX FLOW;

DIGITAL PARTICLE IMAGE VELOCIMETRY; NOTCHED LIFT DISTRIBUTION; TRAILING VORTICES;

WINGS;

EID: 0141461646     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7305     Document Type: Article

References (5)

1. Graham, W. R., "Optimising Wing Lift Distribution to Minimize Wake Vortex Hazard," Aeronautical Journal, Vol. 106, 2002, pp. 413-426.
2. Rossow, V. J., "Lift-Generated Vortex Wakes of Subsonic Transport Aircraft," Progress in Aerospace Sciences, Vol. 35, 1999, pp. 507-660.
3. Crouch, J. D., Miller, G. D., and Spalart, P. R., "Active-Control System for Breakup of Airplane Trailing Vortices," AIAA Journal, Vol. 39, 2001, pp. 2374-2381.
4. Glauert, H., The Elements of Aerofoil and Airscrew Theory, 2nd ed., Cambridge Univ. Press, Cambridge, England, U.K., 1947, Chap. 11.
5. Schmitz, F. W., Aerodynamik des Flugmodells, Tragfluegelmessungen I, 3rd ed., Carl Lange Verlag, Duisburg, Germany, 1957, pp. 89-94.