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Atassi, O., Lichter, S., Bernoff, A., "Vortex Interactions with Boundary Layers Leading to Eruption". AIAA 96-2140, June 1996.

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Caradonna, F. X., Kitaplioglu, C., McCluer, M., Baeder, J. , Leishman, G., Berezin, C., Visintainer, J., Bridgeman, J., Burley, C., Epstein, R., Lyrintzis, A., Koutsavdis, E., Rahrier, G., Delrieux, Y., Rule, J., and Bliss, D., “ A Review of Methods for the Prediction of BVI noise”, AHS Technical Specialists Meeting for Rotorcraft Aeroacoustics and Aerodynamics, October 1997, Williamsburg, VA.

Caradonna, F. X, Henley, E., Silva, M., Huang, S., Komerath, N. M., Mahalingam, R., Reddy, U. C., Funk, R. B., Wong, O., Ames, R., Darden, L. A., Villareal, L., Gregory,J., “Performance Measurement and Wake Characteristics of a Model Rotor in Axial Flight”, to appear in the Journal of the Americal Helicopter Society, April 1998.

Caradonna, F., Henley, E., Silva, M., Huang, S., Komerath N., Reddy, U., Mahalingam, R., Funk, R., Wong, O., Ames, R., Darden, L., Villareal, L., Gregory, J., " An Experimental Study of a Rotor in Forward Flight", presented at the AHS Technical Specialists' meeting for Rotorcraft Acoustics and Aerodynamics, Williamsburg, VA, October 1997.

Cannizzo, F., Lombardi, G., "High Aspect Ratio Wings: Tip Vortex Structure and its Numerical Impications". AIAA 96-1961, June 1996

Chang, Jo won, and Park, Seung O,  "A Experimental Study of Tip Vortex Roll-up of an Oscillating Wing," AIAA Paper 99-0142, 37th AIAA Aerospace Sciences Meeting, Reno, Nevada, Jan. 11-14, 1999.

Cheung, K., Nelson, R., Jumper, E., "A Detailed Experimental Flowfield Study of an Isolated Vortex". AIAA 96-2515, June 1996.

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Conlisk, A. T., “ Modern Helicopter Aerodynamics”, Ann. Rev. of Fluid Mechanics, Vol. 29, 1998m pgs. 515-567.

Darden, L.A., Komerath, N.M., Peterson, K.G., "Roll Control Using a Stagnation Point Actuator". AIAA 96-2498, June 1996.

Devenport, W. J., Rife, M. C., Liapis, S. I., Follin, G. J., “ The Structure and Development of a Wing-Tip Vortex”, J. Fluid Mechanics, 1996, vol. 312, pp. 67-106.

Folin, G., and Devenport, W., "Reynolds Number Effects on Trailing Vortex Structure". AIAA 96-1959, June 1996.

Ghee, T., Berry, J.D., Zori, L.A.J., Elliott, J.W., "Wake Geometry Measurements and Analytical Calculations on a Small-Scale Rotor Model". NASA TP 3584, 1995.

Ghee, T., “ Inboard Sheet Roll-Up of the Wake of a Small-Scale Rotor System ”, Journal of the  American Helicopter Society, Vol. 42, No. 4, pp.383-386, October 1997.

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Han, Leishman, J. G., Coyne, A., " On the Turbulent Structure of a Tip-Vortex Generated by a Rotor", presented at the 52nd AHS Forum, June 1996.

Hariharan, N., PhD. Thesis, School of Aerospace Engineering, Georgia Institute of Technology, 1995. Advisor: Prof. N.L. Sankar

Hinton, D. A., “ Aircraft Vortex Spacing System (AVOSS) Conceptual Design”, NASA-TM 110184, Hampton, VA, Aug. 1995.

Hirschel, E., "Vortex Flows: Some General Properties and Modeling, Configurational and Manipulation Aspects". AIAA 96-2514, June 1996.

Huang, X., Hanff, E., "Surface Flow Topology on a Delta Wing Roling at High Incidence". AIAA 96-2398, June 1996.

Iverson, J. D., Correlation of Turbulent Trailing Vortex Data, J. Aircraft, vol. 13, pp. 338-342, 1976.

Iverson, J. D., Corsiglia, V. R., Park, S., Backhus, D. R. and Brickman, R. A., “ Hot-Wire, Laser Anemometer and Force Measurements of Interacting Trailing Vortices, J. Aircraft, Vol. 16, pp. 448-454, 1979.

Jain, R., Conlisk, A. T., Mahalingam, R. and Komerath, N.M., " Interaction of Tip-Vortices in the Wake of a Two-Bladed Rotor", presented at the 54th Annual Forum of the AHS, May 1998, Washington, D.C.

Kandil, O., Wong, T-C., and Adam, I., "Far-Field Turbulent Vortex-Wake/Exhaust Plume Interaction for Subsonic and HSCT Airplanes". AIAA 96-1962, June 1996.

Kegelman, J.T., and Roos, F.W., "Effects of Leading-Edge Shape and Vortex Burst of a 70-degree-Sweep Delta Wing". AIAA Paper 89-0086, January 1989.

Kim, J. M., Komerath, N. M., and Liou, S. G., “ Vorticity Concentration at the edge of the Inboard Vortex Sheet ”, Journal of the  American Helicopter Society, Vol. 39, No. 2, pp.30-34, April 1994.

Komerath, N.M., Thompson, T.L., Kwon, O.J., and Gray, R.B., "The Velocity Field of a Lifting Model Rotor Blade in Hover". J. Aircraft, 25, 3, 250 - 257, March 1988.

Komerath, N.M., Liou, S-G., Hyun, J-S., "Flowfield of a Swept Blade Tip at High Pitch Angles". AIAA 91-0704, Jan. '91.

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Leibovich, S., "Vortex Stability and Breakdown: Survey and Extension". AIAA Journal, Vol. 22, No. 9, September 1984, pp. 1192-1206.

Leishman, J. G., Baker, A., Coyne, A., " Measurements of Rotor Tip-Vortices Using Three-Component Laser Doppler Velocimetry", presented at the AHS Aeromechanics Specialists' Conference, October 1995.

Leishman, J. G., “ Measurements of the Aperiodic Wake of a Hovering Rotor”, Experiments in Fluids 25 (1998), pp. 352-361.

Lin, S. J., Levy, R., Shamroth, S. J., Govindan, T. R., " A Three-Dimensional Viscous Flow Analysis for the Helicopter Tip Vortex Generation Problem", NASA Contractor Report 3906, August 1985.

Liou, S. G., “ Velocity Measurements on a Lifting Rotor/Airframe Configuration in Low-Speed Forward Flight”, Ph.D. thesis, Georgia Institute of Technology, Atlanta, GA, 1988.

Magness, C., and Roos, F., "The Structure of Forebody Leeward-Side Vortices". AIAA 96-2093, June 1996.

Mahalingam, R., Komerath, N.M., "Rotor Tip Vortex/Airframe Collision Effects on the Vortex and Airframe", AIAA Paper 96-2013, June 1996.

Mahalingam, R., Komerath, N. M., Radcliff, T. D., Burrgraf, O. R., and Conlisk, A. T., “Vortex-Surface Collisions: 3-D Core Flow Effects”, AIAA 97-1785, 28th AIAA Fluid Dynamics Conference, June 1997.

Mahalingam, R., and Komerath, N. M., "Measurements of the Near Wake of a Rotor in Forward Flight", AIAA 98-0692, January 1998.

Mahalingam, R., and Komerath, N. M., "Characterization of the Near Wake of a Helicopter Rotor", AIAA 98-2909, June 1998.

McAlister, K.W., Takahashi, R.K.,"NACA0015 Wing Pressure and Trailing Vortex Measurements". NASA Technical Paper 3151, AVSCOM Technical Report 91-A-003, November 1991.

McAlister, K. W., "Measurements in the Near Wake of a Hovering Rotor". AIAA 96-1958, June 1996.

McAlister, K.W., Schuler, C.A., Branum, L., Wu, J.C., "3-D Wake Measurements Near a Hovering Rotor for Determining Profile and Induced Drag". NASA Technical Paper 3577, ATCOM Technical Report 95-A-006, August 1995.

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Norman, T.R., and Light, J.S.(1987): "Rotor Tip Vortex Geometry Measurements Using the Wide-Field Shadowgraph Technique". Journal of the American Helicopter Society, Vol. 32, No. 2, April 1987, pp. 40 - 50.

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Proctor, F., "Numerical Simulation of Wake Vortices Measured During the Idaho Falls Field Program". AIAA 96-2496, June 1996.

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Ramaprian, B.R., and Zheng, Y., "LDV Measurements in the Roll-Up Region of the Tip Vortex from a Rectangular Wing," AIAA Journal, Vol.35, No.12, Dec 1997, pp.1837-1843.

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Rockwell, D., "Quantitative Imaging of Vortex-Body Interactions". AIAA96-2011, June 1996

Rossow, V., “Wake-Vortex Separation Distances When Flight-Path Corridors are Constrained”, J. Aircraft, Vol. 33, No. 3, May 1996, pp. 539-546.

Rule, J., Bliss, D., "Prediction of Turbulent Trailing Vortex Structure from Basic Loading Parameters". AIAA 96-2495, June 1996.

Rusak, Z., Wang, S., "Review of Theoretical Approaches to the Vortex Breakdown Phenomenon". AIAA 96-2126, June 1996.

Russel, J. W., Sankar, L. N., Tung, C. and Patterson, M. T., " Alterations of the Tip-Vortex Structure from a Hovering Rotor using Passive Tip Devices " , presented at the 53rd AHS Forum, April 1997.

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Sarpkaya, T., “ Decay of Wake Vortices of Large Aircraft”, AIAA Journal, Vol. 36, No. 9, Sept. 1998, pp. 1671-1679.

Savas, O., Jacob, J., Liepmann, D., "Forced Bursting of the Far Wake Vortices of a Rectangular Wing". AIAA 96-2497, June 1996.

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Tsung, Fu-Lin, PhD. Thesis, School of Aerospace Engineering, Georgia Institute of Technology. In progress.

Tung, C., Yu, Y., Low, S., "The Aerodynamic Aspect of Blade/Vortex Interaction". AIAA 96-2010, June 1996.

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Wake, Brian E., PhD Thesis, School of Aerospace Engineering, Georgia Institute of Technology, 1987.

Wendt, B., Reichert, B., "Spanwise Spacing Effects on the Decay of an Array of Axial Vortices". AIAA 96-2518, June 1996.

Winslow, N., and Carroll, B., "Frequency Response of Pressure Sensitive Paints". AIAA 96-1967, June 1996.

Yu, Y. H., “ Rotor Blade-Vortex Interaction Noise : Generating Mechanisms and its Control Concepts”, AHS Specialists meeting on Aeromechanics Technology and Product Design for the 21st Century, October 11-13, 1995, Bridgeport, CT.