[1] J. D. Anderson, Fundamentals of Aerodynamics, McGraw-Hill, Second Edition, 1991.
[2] F. M. Payne, T. T. Ng, R. C. Nelson, L. B. Schiff, Visualization And Flow Surveys of The Leading-Edge Vortex Structure on Delta Wing planforms, AIAA Paper 86-0330, 1986.
[3] F. M. Payne, The Structure of Leading Edge Vortex Flows Including Vortex Breakdown, PhD. Thesis, University of Notre Dame, Deptartment of Aerospace and Mechanical Engineering, Notre Dame, IN, 1987.
[4] M. V. Lowson, the three dimensional vortex sheet Structure on Delta Wing, AGARD CP-438, Fluid Dynamics of Three-Dimensional Turbulent Shear Flows and Transition, 1988.
[5] J. F. Campbell, J. R. Chambers, Patterns In The Sky-Natural Visualization of Aircraft Flow Fields, NASA Langley Research Center, NASA SP-514, 1994.
[6] E. C. Polhamus, Prediction of Vortex- Lift Characteristics by A Leading-Edge Suction Analogy, Journal of Aircraft, Vol. 8, No. 4, pp. 193-199, April 1971.
[7] D. Hummel, on the Vortex Formation over a Slender Wing At Large Incidence, AGARD CP-247, High Angle of Attack Aerodynamics, 1978.
[8] W. H. Wentz, D. L. Kohlman, Vortex Breakdown on Slender Sharp-Edged Wings, Journal of Aircraft, Vol. 8, pp. 156-161,1971.
[9] M. H. Doolabi, H. Ansarian, Computational investigation of mach number and angle attack effects on the flow pattern over a 60o delta wing, Aerosapce Knowledge and Technology Journal, Vol. 3, No. 2, pp. 19-33, Autumn and Winter 2014. (in Persianفارسی )
[10] M. D. Manshadi, M. Feizian, M. Bazzazzadeh, M. Eilbeigi, Evaluation of wing vortex behavior at high angle attack by using laser visualization and numerical method, Aerosapce Knowledge and Technology Journal, Vol. 4, No. 2, pp. 21-33,Winter 2016. (in Persianفارسی )
[11] M. R. Soltani, A. Rajabi, A. Davari Investigation of reduced frequency on vortex and aerodynamics forces on delta wings, The University of Tehran’s Scientific Journal, Vol. 38, Issue 4, Autumn 2004. (in Persianفارسی )
[12] W. H. Wentz, D. L. Kohlman, Vortex Breakdown on Slender Sharp Edged Wings, Journal of Aricraft, Vol. 8, No. 3, 1971, pp. 319-22.
[13] J. T. Kegelman, F. W. Roos, Effects of leading- edge shape and vortex burst on the flow field of a70-degree-sweep delta wing, AIAA paper, January1989.
[14] P. B. Eranshaw, J. A. Law ford, Low-Speed Wind-Tunnel Experiments on a Series of Sharp-Edged Delta Wings, ARC Reports and Memoranda No.3424, March 1964.
[15] J. Rom, High Angle of Attack Aerodynamics, Springer Verlag, New York, 1992.
[16] D. H. Peckham, S. A. Atkinson, Preliminary Results of Low Speed Wind Tunnel Tests on A Gothic Wing of Aspect Ratio 1.0, Report Cp- 508, Aeronautical Research Council, 1957.
[17] B. J. Elle, An investigation at low speed of the flow near the apex of thin delta wings with sharp leading edges, Reports And Memoranda 3176, Aeronautical Research Council, January 1958.
[18] J. Kegelman, F. Roos, Effects of Leading-Edge Shape And Vortex Burst on The Flow Field of A 70 Degree Sweep Delta-Wing, AIAA Paper 89-0086, 1989.
[19] J. Kegelman, F. Roos, The Flow field of Bursting Vortices over Moderately Swept Delta Wings, AIAA Paper, 1990.
[20] J. M. Delery, Aspects of Vortex Breakdown, Progress in Aerospace Sciences, Vol.30, pp. 1-59, 1994.
[21] F. M. Payne, T. T. Ng, R. C. Nelson, Visualization and Flow Surveys of the Leading Edge Vortex Structure on Delta Wing Planforms, AIAA Paper, 1986.
[22] A. M. Mitchell, D. Barberis, J. Delery, Oscillation of Vortex Breakdown Location & Its control by Tangential Blowing, AIAA Paper 98-2914, 1998.
[23] N. C. Lambourne, D. W. Bryer, the Bursting of Leading-Edge Vortices–Some Observations and Discussions of the Phenomenon, Reports and Memoranda 3282, Aeronautical Research Council, 1962.
[24] F. M. Payne, T. T. Ng, R. C. Nelson, Experimental Study of the Velocity Field on a Delta Wing, AIAA Paper 87-1231, June 1987.
[25] D. I. Greenwell, Pitfalls in Interpretation of Delta Wing Flow Visualization, NATO RTO Symposium on Advanced Flow Management, Leon, Norway, RTO MP–069(I)–(SYA)-05, 2001.
[26] C. Gibbs, A. Sethna, I. Wang, D. M. Tang, E. H. Dowell, Aeroelastic Stability of a cantilevered Plate in Yawed Subsonic Flow, Journal of Fluids Structure, Vol. 49, pp. 450-462, 2014.
[27] D. M. Tang, E. H. Dowell, Computational/Experimental Aeroelastic Study for a Horizontal Tail Model with Freeplay, AIAA Journal, Vol. 51, pp. 341-352, 2013.
[28] D. M. Tang, E. H. Dowell, Effects of a Free-to-Roll Fuselage on Wing Flutter, Theory and Experiment, AIAA Journal, 52, pp. 2625-2632, 2014.
[29] D. M. Tang, E. H. Dowell, Experimental Aerodynamic Response for an Oscillating Airfoil in Buffeting Flow, AIAA Journal, Vol. 52, pp. 1170–1179, 2014.
[30] D. M. Tang, E. H. Dowell, Experimental Aeroelastic Response for a Freeplay Control Surface in Buffeting Flow, AIAA Journal, Vol. 51, pp. 2852–2861, 2013.
[31] F. Besem, J. D. Kamrass, J. P. Thomas, D. M. Tang, R. E. Kielb, Vortex-Induced Vibration and Frequency Lock-in of an Airfoil at High Angles of Attack, Journal of Fluids Engineering Trans. ASME, Vol. 138, 2016.
[32] A. Khrabrov, D. Greenwell, TsAGI 70° and 65° Delta Wings Test Cases, RTO-TR-AVT-080, Chapter 9, 2014.
[33] L. Zhitao, J. Yubiao, H. Yong, Experimental Research on Unsteady Vortex Separation and Control about a Delta-Wing-Body Combination, 10th International Conference on Fluid Control, Measurements and Visualization, Moscow, Russia, August 17-21, 2009.
[34] J. M. Brandon, G. H. Shah, Effect of lager amplitude pitching motions on the unsteady aerodynamic characteristics of flat-plate wings, AIAA Paper, August 1988.