Effects of canard position on wing surface pressure

Scientia Iranica

Volumn 17, Issue 2 B, 2010, Pages 136-145

  Soltani, M R ^a   Askari, F ^a   Davari, A R ^b   Nayebzadeh, A ^a  

^a SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

^b ISLAMIC AZAD UNIVERSITY   (Iran)

Author keywords

Canard; Delta wing; Downwash; Leading edge vortex

Indexed keywords

ANGLE OF ATTACK; FLOW FIELDS; VORTEX FLOW; WIND TUNNELS; WINGS;

CANARD; CANARD CONFIGURATION; DELTA WINGS; DOWNWASH; HIGH ANGLES OF ATTACK; LEADING-EDGE VORTICES; VERTICAL POSITIONS; WIND TUNNEL TESTS;

DELTA WING AIRCRAFT;

EXPERIMENTAL STUDY; FLOW FIELD; SURFACE PRESSURE; VORTEX; WIND FIELD; WIND TUNNEL;

EID: 77952819204     PISSN: 10263098     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (13)

1. Ashraf, A. Omar, Sri, S. "Experimental investigation of incompressible flow around delta wing-slender body combinations", International Journal of Applied Engineering Research (IJAER), 2(4), pp. 685-698 (2007)
2. Wei-Jen, S., Curtis, W. "Aerodynamic characterization of a canard guided artillery projectile", AIAA 2007-672 (2007).
3. Pandya, S.A. and Aftofmis, M.J. "Computation of external aerodynamics for a canard rotor/wing aircraft", AIAA 2001-0997 (2001).
4. Howard, R.M. and O'Leary, J. "Flow field study of a close-couple canard configuration", AIAA Journal, 31(4), pp. 908-914 (1994).
5. Eaxnshaw, P.B. and Lawford, I.A. "Low-speed wind tunnel experiments on a series of sharp-edged delta wings", Aeronautical Research Council, RM 3424 (1964).
6. Erickson, G.E. "Water-tunnel studies of leading-edge vortices", Journal of Aircraft, 19(6), pp. 442-448 (1982).
7. Seginer, A. and Salomon, M. "Performance augmentation of a 60-degree delta aircraft configuration by spanwise blowing", Journal of Aircraft, 23(2), pp. 801-807 (1986).
8. Wood, N.I. and Roberts, L. "Control of vortical lift on delta wings by tangential leading-edge blowing", Journal of Aircraft, 25(3), pp 236-243 (1988).
9. Lee, M. and Ho, CM. "Lift force of delta wings", Applied Mechanics Review, 43(9), pp 109-221 (1990).
10. Hummel, H. and Oelker, H.C. "Low-speed characteristics for the wing-canard configuration of the international vortex flow experiment", Journal of Aircraft, 31(4), pp 868-878 (July-Aug. 1994)
11. Rae, H.W., Jr. and Pope, A., Low-Speed Wind Tunnel Testing, John Wiley & Sons, Inc. (1984)
12. Thomas, G.B., Roy, D.M. and John, H.L.V., Mechanical Measurements, Addison-Wesley Publishing Company (1993)
13. Nayebzade, A. "An experimental survey on the effects of canard position on the flowfield over the wing in subsonic flow", Msc. Thesis, Sharif University of Technology (Jan. 2008)