Investigation of the unsteady pressure fluctuations on an F/A-18 wing at high incidence

Journal of Aircraft

Volumn 33, Issue 5, 1996, Pages 888-894

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

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

^b UNIVERSITY OF OTTAWA   (Canada)

^c Exp Aerodynamics and Aeroelasticity ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRCRAFT MODELS; CORRELATION METHODS; DYNAMIC RESPONSE; FIGHTER AIRCRAFT; FLOW VISUALIZATION; FRICTION; MATHEMATICAL MODELS; PRESSURE MEASUREMENT; PRESSURE TRANSDUCERS; UNSTEADY FLOW; WIND TUNNELS;

ANGLE OF ATTACK; CROSS CORRELATION; MACH NUMBERS; UNSTEADY PRESSURE FLUCTUATIONS;

WINGS;

EID: 0030246081     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47031     Document Type: Article

References (8)

1. Fisher, D. F., Del Frate, J. H., and Richwine, D. M., "In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack," NASA TM 4193, May 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 α = 30 Deg," Journal of 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 Paper 95-1865, June 1995.
4. Lee, B. H. K., and Marineau-Mes, S., "Mach Number and Angle of Attack Effects on the Flow Past a Fighter-Type Wing at High Incidence," AIAA Paper 96-2510, June 1996.
5. Lee, B. H. K., and Brown, D., "Wind-Tunnel Studies of F/A-18 Tail Buffet," Journal of Aircraft, Vol. 29, No. 1, 1992, pp. 146-152.
6. Erickson, G. E., Hall, R. M., Banks, D. W., Del Frate, J. H., Schriener, J. A., Hanley, R. J., and Pulley, C. T., "Experimental Investigation of the F/A-18 Vortex Flows at Subsonic Through Transonic Speeds, Invited Paper," AIAA Paper 89-2222, July 1989.
7. Rabiner, L. R., Schafer, R. W., and Dlugos, D., "Chapter 2.1, Periodgram Method for Power Spectrum Estimation," "Chapter 2.3, a Coherence and Cross Spectral Estimation Program," Programs for Digital Signal Processing, edited by the Digital Signal Processing Committee, IEEE Acoustics, Speech and Signal Processing Society, Inst. of Electrical and Electronics Engineers, New York, 1979.
8. Hwang, C., and Pi, W. S., "Investigation of Steady and Fluctuating Pressure Associated with the Transonic Buffeting and Wing Rock of a One-Seventh Scale Model of the F-5A Aircraft," NASA CR 3061. Nov. 1978.