Physical mechanisms of lift enhancement for flexible delta wings

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 14407-14419

  Vardaki, E ^a,b,c   Gursul, I ^a,b,c   Taylor, G S ^a,b,c  

^a UNIVERSITY OF BATH   (United Kingdom)

^b Department of Mechanical Engineering ^*  (United Kingdom)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS; NATURAL FREQUENCIES; PRESSURE EFFECTS; VIBRATIONS (MECHANICAL); VORTEX FLOW; WINGS;

FLEXIBLE NONSLENDER DELTA WINGS; LIFT ENHANCEMENT; PRESSURE GRADIENT;

LIFT;

EID: 30744434106     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-867     Document Type: Conference Paper

References (8)

1. nd Flow Control Conference, 28 June-1 July 2004, Portland, Oregon.
2. rd Aerospace Sciences Meeting and Exhibit Conference, 10-13 January 2005,Reno,NV.
3. Gursul, I., Survey Article: "Review of Unsteady Vortex Flows over Slender Delta Wings", Journal of Aircraft, in print.
4. Traub, L. W., "Lift Prediction of Spanwise Cambered Delta Wings", Journal of Aircraft, Vol. 36, No. 3, pp. 515-522, May-June 1999.
5. Taylor, G.S., Schnorbus, T., and Gursul, I., "An Investigation of Vortex Flows over Low Sweep Delta Wings", AIAA-2003-4021, AIAA Fluid Dynamics Conference, 23-26 June, Orlando, FL.
6. Taylor, G. and Gursul, I., "Buffeting Flows over a Low Sweep Delta Wing", AIAA Journal,vol.42, no 9, September 2004, pp. 1737-1745.
7. Gordnier, R. E. and Visbal, M. R., "Higher-Order Compact Difference Scheme Applied to the Simulation of a Low Sweep Delta Wing Flow", AIAA 2003-0620, 41st AIAA Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno, NV.
8. Roos, F.W. and Kegelman, J.T., "Control of Coherent Structures in Reattaching Laminar and Turbulent Shear Layers", AIAA Journal, vol. 24, no. 12, December 1986, pp. 1956-1963.