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May 1978.
4Werle, H., "Flow \nsualhation Technique for the Study of High Incidence Aerodynam-
ics:' LS-121, AGARD, Paper 3, 1982.
5Johnson, T. D., Jr., and Huffman, J. K, "Experimental Study of Vortex Flaps on a Delta
Wing Sweep Series at High Angles of Attack:' NASA CP-2416, Vol. 11, 1985, pp. 169-184.
6Campbell, J. F., and Osbom, R. F., "Leading-Edge Vortex Research, Some Nonplanar
Concepts and Current Challenges," NASA CP-2416, 1992, pp. 31-64.
7Hunt, B. L., tiAsymmetric Vorkx Forces and Wakes on Slender Bodies:' (Invited Paper)
AIAA Paper 82-1336, Aug. 1982.
RPayne, F. M., and Nelson, R. C., "An Experimental Study of Vortex Breakdown on a
Delta Wing:' NASA CP-2416, 1992, pp. 135-161.
9Skow, A. M., TiMga, A., Jr., and Moore, W. A., "Forebody-Wing Vortex Interactions
and their Influence on Departure and Spin Resistance," CP-247, AGARD, Paper No. 6,
1979.
IoWent.z, W. H., and Kohlman, D. L., "Vortex Breakdown on Slender Sharp-Edged Wings:'
Journal of Aircraft, Vol. 3, March 1971.
iJ Roos, F. W., and Kegelman, J. T., "Leading Edge Vortex Flow Fields:' NASA CP-3149,
Part 1, 1990, pp. 157-172.
12Skow, A. M., and Erickson, G. E., "Modem Fightef Design for High-Angle-of-Attack
Maneuvering:' LS 121, AGARD, Paper 4, 1982.
1311iorripson, D. H., "A Visuajisation Study of the Vortex Flow Around Double-Delta
Wings:' Australian Dept. of Defence, Aerodynamics Rept. 165, Melbourne, Australia, Aug.
1985.
14Hall, R. M., Erickson, G. E*, Banks, D. W., and Fisher, D. F., "Advances in High Alpha
Experimental Aerodynamics: Ground Test and Flight:' NASA CP-3149, Part l, Vol. 1, 1990,
pp. 69-87.
lsRao,D. M.,"Pneumatic Concept for rfip_StaU ControlofCranked Arrow Wings," Journal
of Aircraft, Vol. 31, No. 6, Nov: Dec. 1994, pp. 1380-1386.
STABILITY AND CONTROL PROBLEMS AT HIGH ANGLES OF ATTACK 751
16Behrbohm, H., "Basic Low Speed Aerodynamics of ffie Short Coupled Canard Config-
uration of Small Aspect Ratio:' Svenska Aeroplan Aktiebolag, SAAB TN 60, Linkoping,
Sweden, July 1965.
riHoward, R. M., and Kersh, J. M., Jr., "Effect of Canard Deflection on Enhanced Lift for
Close-Coupled Canard Configuration:' AIAA Paper 91-3222, Sept. 1991.
18Lamont, P. J., **Pressure Measurements on an Ogive-Cylinder at High Angles of Attack
with Laminar, Transitional and Turbulent Separation:' AIAA Paper 80-1556, Jan. 1980.
19Mendenhall, M. R., and Nielsen, J. N., "Effect of Symmetrical Vortex Shedding On
the Longitudinal Aerodynamic Characteristics of Wing-Body-Tail Combinations," NASA
CR-2473,1975.
20Headley, J. W., tiAnalysis of Wind Tunnel Data Pertaining to High-Angle-of-Attack
Aerodynamics," Vol. I-Techrucal Discussion and Analysis of Results, Air Force Flight
Dynamics Laboratory, AFFDL-TR-78-94, Wright-Patterson Air Force Base, OH, July
1978.
21:Levin, D., and Katz, J., "Selflnduced Roll Oscillations ofLow AspeclRatio Rectangular
Wings:' AIAA Paper 90-2811. 1990.
22Chambers, J. R.,l*High-Angle-of-Attack Aerodynamics: Lessons Leamed," AIAA Paper
86-1774, 1986.
230rlick-Rueckrnann, W. J., "Aerodynamic Aspects of Aircraft Dynanucs at High Angles
of Attack:' Journal of Aircraft, Vol. 20, No. 9, 1983, pp. 737-752.
24Nguyen, L. T., Yip, L. P., and Chambers, J. R., "Self Induced Wing Rock of Slender
Delta Wings," AIAA Paper 81 1883, Aug. 1981.
25Ross, A. J., "Investigation ofNonlinear Motion Experienced on a Slender-Wing Research
Aircraft:' Jorrrnal of Aircraft, Vol. 9, No. 9, 1972, pp. 625-631.
26Schnudt, L. V., "Wing Rock due to Aerodynamic Hysteresis," Journal of Aircraft, Vol.
16, 1979, pp. 129-133.
21Levin, D., and Katz, J., "Dynamic Load Measurements with Delta Wings Undergoing
SelfInduced Roll Oscillations:' Journal of Aircraft, Vol. 21, No. 1, 1984, pp. 30-36.
2SEricson, L. E., "The Fluid Mechanics of Slender Wing Rock:' Journal of Aircraft, Vol.
21, No. 5, 1984, pp. 322-328.
2sNguyen, L. T., Whipple, R. D., and Brandon, J. M., "Recent Experiences of Unsteady
Aerodynanuc Effects on Aircraft Flight Dynamics at High-Angles-of-Attack:' Paper 28,
CP 386, AGARD, 1985.
30Jun, Y. W., and Nelson, R. C., "Leading-Edge Vortex Dynamics on a Slender Oscillating
\Ning:' Joumal of Aircraft, Vol, 25, No. 9, 1988, pp. 815-819.
31Arena, A. S., and Nelson, R. C., "Experimental Investigations on Limit Cycle Wing Rock
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