Effects of Gurney flaps on the lift enhancement of a cropped nonslender delta wing

Experiments in Fluids

Volumn 32, Issue 1, 2002, Pages 99-105

  Li, Y C ^a   Wang, J J ^a   Tan, G K ^a   Zhang, P F ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CALCULATIONS; DRAG; LIFT; PRESSURE EFFECTS; REYNOLDS NUMBER; TESTING; WIND TUNNELS;

CROPPED NONSLENDER DELTA WING; GURNEY FLAPS; LIFT COEFFICIENTS; LIFT TO DRAG RATIO;

WINGS;

EID: 0036240884     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480200010     Document Type: Article

References (15)

1. Design of subsonic airfoils for high lift
2. A water tunnel study of Gurney flap
3. Lift enhancement of an airfoil using a Gurney flap and vortex generators
4. Computational evaluation of an airfoil with a Gurney flap
5. The effect of Gurney flaps on a NACA0011 Airfoil
6. Gurney flap effects and scaling for low-speed airfoils
7. Gurney flap experiments on airfoils, wings, and reflection plane model
8. An experimental investigation of Gurney flaps on a GA(W)-2 airfoil with 25% slotted flap
9. Experimental investigation of Gurney flaps on a two-element general aviation airfoil
10. Experimental study of lift-enhancing tabs on a two-element airfoil
11. Lift-enhancing tabs on multielement airfoils
12. Navier-Stokes analysis of lift-enhancing tabs on multi-element airfoils
13. Wind-tunnel investigations of wings with serrated sharp trailing edges
14. Gurney flap experiments of airfoil and wings
15. Lift augmentation on a delta wing via leading edge fences and the Gurney flap