Transonic evaluation of a pneumatic spoiler for aircraft control

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages

  Walchli, Lawrence A ^a   Langan, Kevin J ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; ASPECT RATIO; MACH NUMBER; PNEUMATICS; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT; SWEPT WINGS; TRANSONIC AERODYNAMICS;

AIR INJECTION; CIRCULATION CONTROL WINGS; COEFFICIENT VALUES; EXPERIMENTAL INVESTIGATIONS; HIGH-ASPECT RATIO WING; LOCKHEED MARTIN; PITCHING MOMENTS; TRAILING EDGES;

AERODYNAMICS;

EID: 84964296749     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Peake, D. J., et al, “Transonic Lift Augmentation of Two-Dimensional Supercritical Aerofoils by Means of Aft Camber, Slot Blowing and Jet Flaps in High Reynolds Number Flow”, ICAS Paper #74-11, The Ninth Congress of the International Council of Aeronautical Sciences, August 1974.
2. Haight, C. H. and Mask, R. L., “Transonic Maneuver/Cruise Airfoil Design Employing Active Diffusion Control”, Viscous Flow Drag Reduction. Progress in Astronautics and Aeronautics, Vol. 72, ALAA, pp. 187-211, 1980.
3. Grahame, W. E. and Headley, J. W., “Experimental Investigation of Boundary Layer Control (BLC) Devices at Transonic Speeds”, AFFDL-TR-70-22, Vol. 1 April 1970.
4. Stewart, V. R., “Aerodynamic Characteristics of a Propulsive Wing/Canard Concept at STOL Speeds”, NASA CR 177982, November 1985.
5. Ely, W. L. and Berrier, F. C., “Performance of Steady and Intermittent Blowing Jet Flaps and Spanwise Upper Surface Slots”, AFFDL-TR-75-128, November 1975.
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7. Simon, J. M., et al., “Results of Exploratory Wind Tunnel Tests of F-16/VISTA Forebody Control Devices”, WL-TR-93-3013, January 1993.
8. Albright, A. E., “Analysis Report of 1/9-Scale F-16 Forebody Vortex Control Model Test LLST 9313”, Lockheed Fort Worth Company Report FZT-613, February 1994.
9. Walchli, L. A. and Moorhouse, D. J., “Forebody Vortex Control”, AGARD-CP-593-17, December 1997.
10. Skow, A. M. and Peake, D. J., “Control of the Forebody Vortex Orientation by Asymmetric Air Injection”, AGARD-CP-262-24, May 1979.
11. Cornelius, K. C., et al., “An Experimental Study of Pneumatic Vortex Flow Control on a High Angle-Of-Attack Forebody Model”, AIAA 92-0018, January 1992.
12. Luria, F., “Wind Tunnel Tests of a 1/8-Scale X-29 Forebody Model Incorporating Blowing”, USAF WL- TM-91-327, December 1991.
13. Smith, W. R Capt, USAF, “X-29 High Angle-Of- Attack Flight Test Program”, Volume 5, X-29 A-2 High Angle-Of-Attack Flight Test Results, November 1993
14. Mosbarger, “Pneumatic Aerodynamic Device Development (PADD): An Evaluation”, WL-TR-96-3101, June 1996.
15. Englar, R. J., et al., “Pneumatic Aerodynamic Flexible Skin Lift and Control Devices”, AFRL-VA-WP-TR-1998-3074, January 1998