Wind tunnel tests of delta wings with antisymmetric leading edge flap deflections

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Ize, Carlos ^a   Arena, Andrew S ^a  

^a Oklahoma State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; DELTA WING AIRCRAFT; PRESSURE DISTRIBUTION; VORTEX FLOW; WIND TUNNELS;

ANGLES OF ATTACK; CONTROL EFFECTIVENESS; FLOW DISTRIBUTION; HIGH ANGLES OF ATTACK; LEADING EDGE FLAPS; LEADING-EDGE VORTICES; ROLL MOMENT COEFFICIENTS; WIND TUNNEL TESTS;

WINGS;

EID: 84983187984     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-990     Document Type: Conference Paper

References (12)

1. Rinoie, K. and Stollery, J.L., "Experimental Studies of Vortex Flaps and Vortex Plates", Journal of Aircraft, Vol. 31, No. 2, March-April 1994, pp. 322-329.
2. Marchman, J.FPlentovich, E.B., and Manor, D., "Performance Improvement of Delta Wings at Subsonic Speeds Due to Vortex Flaps", AIAA Paper 80-1802, AIAA Aircraft System Meeting, Anaheim, California, August 4-6, 1980.
3. Marchman, J.F., "Effectiveness of Leading-Edge Vortex Flaps on a 60 and 75 Degree Delta Wing", Journal of Aircraft, Vol.18, No.4, 1981,pp.280-286.
4. Marchman, J.F., and Thomas, R.H., "Effects of Yaw on Leading Edge Vortex Flap Aerodynamics", AIAA Paper 81-1660, AIAA Aircraft Systems and Technology Conference, Dayton, Ohio, August 11-13,1981.
5. Levin, D., and Seginer, A., "Experimental Investigation of Vortex Flaps on Thick Delta Wings", Journal ofAircraft. Vol.31, No.4, 1994, pp.988-991.
6. Walton, J., and Katz, J., "Reduction of Wing Rock Amplitudes Using Leading Edge Vortex Manipulations", AIAA-Paper 92-0279, 30th Aerospace Sciences Meeting & Exhibit, January 6-9, Reno, NV, 1992.
7. Roberts, S.D. and Arena, Jr., A.S., " An Inviscid Model for Evaluating Wing Rock Suppression Methodologies", AIAA 94-0808, 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994, Reno, NV.
8. Ize, C. and Arena, Jr., A.S., " Effects of Asymmetric Leading Edge Flap Deflection on Delta Wings in Roll", AIAA Paper 97-3486, Atmospheric Flight Mechanics Conference, August 11-13, New Orleans, Louisiana, 1997.
9. Hummel, I.D., "On the Vortex Formation Over a Slender Wing at Large Angles of Incidence", AGARD CP-247, 1978.
10. Carcaillet, R., Manis, F., Pagan, D., and Solignac, J.L., "Leading Edge Vortex Flow Over a 75 Degree-Swept Delta Wing-Experimental and Computational Results", ICAS, Sept. 1986, 15 pg.
11. Ize, C, "Effects of Asymmetric Leading Flap Deflection on Delta Wings", Ph.D. Thesis, Department of Mechanical and Aerospace Engineering, Oklahoma State University, July 1998.
12. Marchman, J.F., "Aerodynamics of Inverted Leading-Edge Flaps on Delta Wings", Journal o f Aircraft, Vol.18, No.12, 1981, pp.1051-1056.