Mach number and angle of attack effects on the flow past a fighter-type wing at high incidence

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 1062-1076

  Lee, B H K ^a   Marineau Mes, S ^b  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

^b UNIVERSITY OF OTTAWA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK INDICATORS; DYNAMIC LOADS; FLOW SEPARATION; LIFT; MACH NUMBER; RIGID WINGS; TINNING; VORTEX FLOW;

ANGLES OF ATTACK; FLOW SEPARATION AND REATTACHMENTS; HIGH INCIDENCE; HIGH-LIFT DEVICES; NONLINEAR STATICS; PRESSURE DIFFERENCES; STATIC AND DYNAMIC LOADS; SURFACE FLOW VISUALIZATION;

ANGLE OF ATTACK;

EID: 84964240154     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-2510     Document Type: Conference Paper

References (8)

1. Fisher, D.F., Del Frate, J.H., Richwine, D.M., “In-FlightFlow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack”, NASA TM 4193, 1990.
2. Lee, B.H.K., Valerio, N.R. and Tang, F.C., “Steady and Unsteady Pressure Distributions on an F/A-18 Wing at a = 30 Deg”, J. Aircraft Vol. 31, No. 4, 1994, pp. 862-867.
3. Lee, B.H.K. and Marineau-Mes, S., “Investigation of the Unsteady Pressure Fluctuations on an F/A-18 Wing at High Incidence”, AIAA-95-1865, AIAA 13th Applied Aerodynamics Conference, June 19-22, 1995, San Diego, CA.
4. Frazier, FA., “F-18 Hornet - LEX fence flight test results”, Society of Experimental Test Pilots' Symposium, Beverley Hills, CA, October 1988.
5. Lee, B.H.K. and Marineau-Mes, S., “The Unsteady Pressure Field on a Wing with Large Regions of Separated Flow”, Paper ICAS-96-1.6.3, International Congress of the Aeronautical Sciences, Sorrento, Italy, 8-13 Sept. 1996.
6. Lee, B.M.K. and Brown, D., “Wind-Tunnel Studies of F/A-18 Tail Buffet”, J. Aircraft Vol. 29, No. 1, 1992, pp.146-152.
7. Erickson, G.E., Hall, R.M., Banks, D.W., DelFrate, J.H., Schriener, J.A., Hanley, R.J. and Pulley, C.T., “Experimental Investigation of tlie F/A-18 Vortex Flows at Subsonic Through Transonic Speeds, Invited Paper”, AIAA 89-2222. AIAA 7th Applied Aerodynamics Conference, Seattle. WA.. July 31-Aug. 2. 1989.
8. Hoffman, J.J. and Doligalski, T.L. “Initial Development of a Low-Speed Jet in Cross-Flow”, AIAA 85-1619, AIAA 18th Fluid Dynamics and Plasmadynamics and Laser Conference, Cincinatti, OH, July 16-18, 1985.