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【1】       Ericsson, L.E. and Reding, J.P., “Vortex-Induced Asymmetric Loads in 2-D and 3-D Flows,” AIAA-80-0181, January 1980
【2】       Chapman, G.T., Keener, E.R., and Malcolm, G., ”Asymmetric Aerodynamic Forces on Aircraft Forebodies at High Angle of Attack – Some Design Guides,” Paper No.16, AGARD Meeting on Stall/Spin Problems of Millitary Aircraft, Ames Rearch Center, Moffett Field, California, November 18-21,1976

【3】       Wardlaw, A.B., Jr., “High Angle of Attack Missile Aerodynamics,” Paper 5, AGARD LS-98, March 1978

【4】       Peake, D.J. and Tobak, M., “Three Dimensional Interactions and Vortical Flows with Emphasis on High Speeds, AGARD-ograph, March 1980

【5】       Skow, A.M. and Ericsson, G.E., “Modern Fighter Aircraft Design for High Angle of Attack,” AGARD Lecture Series No.121, High-Angle-Of-Attack Aerodynamics, March 1982

【6】       Ericsson, L.E., Sources of High Alpha Vortex Asymmetry at Zero Sideslip, J.Aircraft,1992, Vol.29, No.6, P1086~1090

【7】       Lamont, P.J., Pressures around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent  Separation, AIAA Journal, 1980, Vol.20, No.11, P1492~1499

【8】       Degani, D., Numerical Investigation of the Origin of Vortex Asymmetry, AIAA Paper 90-0593

【9】       David Degani, Instability of Flow over Bodies at Large Incidence, AIAA journal,1992

【10】   Keener  ER. Flow-Separation Patterns on Symmetric Forebodies. NASA TM-86016,1986

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