Soheil Mohtaram, Mohammad Amin Nikbakht, Detect Tool Breakage by Using Combination Neural Decision System & Anfis Tool Wear Predictor, International Journal of Mechanical Engineering and Applications. Vol. 1, No. 2, 2013, pp. 59-63.
 Staelens, Y.D., R.F. Blackwelder, and M.A. Page. Novel Pitch Control Effectors for a Blended Wing Body Airplane in Takeoff and Landing Configuration. in 45th AIAA Aerospace Sciences Meeting and Exhibit 8-11 January 2007, Reno, Nevada. AIAA 2007-68.
 Abas MFB, Rafie ASBM, Yusoff HB, et al. Flapping wing micro-aerial-vehicle: Kinematics, membranes, and flapping mechanisms of ornithopter and insect flight[J]. Chinese Journal of Aeronautics, 2016, 29(5) : 1159-1177.
 McLain, B.K., steady and unsteady aerodynamic flow studies over a 1303 ucav configuration. September 2009, naval postgraduate school.
 A. Gilliot , S.M., et al. Static and Dynamic SACCON PIV tests , Part І: Forward Flowfield. in 28th AIAA Applied Aerodynamics Conference 28 June-1 July 2010, Chicago, Illinois. AIAA 2010-4395.
 Sirohi, Jayant. "Chapter 5 - Bioinspired and Biomimetic Microflyers." Engineered Biomimicry (2013): 107-138.
 Robert, K., et al. Static and Dynamic SACCON PIV Tests, Part II: Aft Flow Field. in 28th AIAA Applied Aerodynamics Conference 28 June-1 July 2010, Chicago, Illinois. AIAA 2010-4396.
 Robert, C.N. and P. Alain, The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers. Aerospace Sciences, 2003: p. 185–248.
 Filippone A. Flight Performance of Fixed and Rotary Wing Aircraft[J]. 2006.
 Schutte, A., D. Hummel, and S. M. Hitzel. Numerical and experimental analyses of the vortical flow around the SACCON configuration. in 28th AIAA Applied Aerodynamics Conference 28 June-1 July 2010, Chicago, Illinois. AIAA 2010-4690.
 Jani JM, Leary M, Subic A, et al. A review of shape memory alloy research, applications and opportunities[J]. Materials & Design, 2014, 56(4):1078-1113.
 Gursula, I., R. Gordnierb, and M. Visbal, Unsteady aerodynamics of nonslender delta wings. Aerospace Sciences, 2005. 41: p. 515–557.
 Steven, D.R. and S.A. Andrew, An Inviscid Model for Evaluating Wing Rock Suppression Methodologies, in 32nd Aerospace Sciences Meeting & Exhibit January,Reno. AIAA 94-0808, 1994.
 Kramer, M., Increase in the maximum lift of an airfoil due to a sudden increase in its effective angle of attack resulting from a gust. NASA TM-678, 1932.
 Harris, F.D. and R.R. Pruyn, Blade Stall Half Fact, Half Fiction. J. Am. Helicopter Soc.13, (1968) 27–48.
 Ham, N.D. and M.S. Garelick, Dynamic stall considerations in helicopter rotors. J.Am. Helicopter Soc. 13, (1968) 49–55.
 Choudhry, A., M. Arjomandi, and R. Kelso, Horizontal axis wind turbine dynamic stall predictions based on wind speed and direction variability. Mech. Eng., Part A: J. Power Energy 227, (2013) 338–351.
 Ferreira, C.S., G.v.B. G. van Kuik, and F. Scarano, Visualization by PIV of dynamic stall on a vertical axis wind turbine. Exp. Fluids 46 (2009) 97–108.
 Schreck, S. and M. Robinson, Blade three-dimensional dynamic stall response to wind turbine operating condition. J. Sol. Energy Eng. 127, (2005) 488.
 Schreck, S., et al., HAWT dynamic stall response asymmetries under yawed flow conditions. Wind Energy 3, (2000) 215–232.
 Shipley, D.E., et al., Evidence that aerodynamic effects, including dynamic stall,dictate HAWT structural loads and power generation in highly transient time frames, in National Renewable Energy Lab,. 1994: United States.
 Shipley, D.E., M.S. Miller, and M.C. Robinson, Dynamic stall occurrence on a horizontal axis wind turbine blade, in National Renewable Energy Lab. 1995: United States.
 Carr, L.W., Progress in analysis and prediction of dynamic stall, . J. Aircr.25, (1988) 6–17.
 Ekaterinaris, J.A. and M.F. Platzer, Computational prediction of airfoil dynamic stall. Aerosp. Sci. 33 (1998) 759–846.
Kerho, M.F., Adaptive airfoil dynamic stall control. J. Aircr. 44 (2007) p. 1350–1360.
 Krzysiak, A., Improvement of helicopter performance using self-supplying air jet vortex generators. J. KONES Powertrain Transp, (2013) 20.
 Leishman, J. and T. Beddoes, A semi-empirical model for dynamic stall,. J. Am.Helicopter Soc. 34, (1989): p. 3–17.
 McCroskey, W., The Phenomenon of Dynamic Stall. DTIC Document, 1981.
 McCroskey, W.J., Unsteady airfoils. (1982) Annu. Rev. Fluid Mech. 14. p. 285–311.
 Liu, H. and K. Kawachi, A numerical study of insect flight. J. Comput. Phys. 146, (1998) 124–156.
 Wang, Z.J., Vortex shedding and frequency selection in flapping flight. J. Fluid Mech. 410 (2000) p. 323–341.
 Gheisari, R., et al. "Experimental studies on the ultra-precision finishing of cylindrical surfaces using magnetorheological finishing process." Production & Manufacturing Research 2.1 (2014): 550-557.
 Shyy, W., et al., Aerodynamics of Low Reynolds Number Flyers. Cambridge University Press, 2007.
Norberg, U.M.L., Structure, form, and function of flight in engineering and the living world. J. Morphol. 252, (2002) p. 52–81.
 Lang, J.D. and M.S. Francis, Unsteady Aerodynamics and Dynamic Aircraft Maneuverability. DTIC Document, 1985.
 Niu, Y.-Y. and C.-C. Chang, How do aerodynamic forces of the pitching rigid and flexible airfoils evolve? AIAA J, (2013) p. 1–7.
 Visbal, M.R., Dynamic stall of a constant-rate pitching airfoil. J. Aircr. 27 (1990): p. 400–407.
 Karim, M.A. and A. Mukund, Suppression of Dynamic-Stall Vortices over Pitching Airfoils by Leading-Edge Suction. AIAA, August 1994. 32.
 Lars, E.E. and J.P. Reding, Dynamic Stall at High Frequency and Large Amplitude. J. AIRCRAFT. 17: p. 136-142.
 Francis, M.S. and J.E. Keesee, Airfoil Dynamic Stall Performance with Large-Amplitude Motions. AIAA. 23.
 Lawrence, W.C., Progress in Analysis and Prediction of Dynamic Stall. AIRCRAFT, january 1988. 25: p. 6-17
 Mohtaram, Soheil, et al. "Energy-exergy analysis of compressor pressure ratio effects on thermodynamic performance of ammonia water combined cycle." Energy Conversion & Management 134(2017):77-87.
 Mohtaram, Soheil, et al. "Evaluating the effect of ammonia-water dilution pressure and its density on thermodynamic performance of combined cycles by the energy-exergy analysis approach." Mechanics 23.2 (2017): 209-219.
 Anderson, J.D., Fundamentals of Aerodynamics. 2001., New York: McGraw-Hill.
 Leishman, J., Dynamic stall experiments on the NACA 23012 aerofoil. Exp.Fluids 9, 1990: p. 49–58.
 Gupta, S. and J.G. Leishman, Dynamic stall modelling of the S809 aerofoil and comparison with experiments. Wind Energy 9, (2006): p. 521–547.
 Digavalli, S.K., Dynamic Stall of a NACA 0012 Airfoil in Laminar Flow. 1994., Massachusetts Institute of Technology.
 Jumper, E., S. Schreck, and R. Dimmick, Lift-curve characteristics for an airfoil pitching at constant rate. J. Aircr. 24, (1987) p. 680–687.
 Ramsay, R.R., M.J. Hoffmann, and G.M. Gregorek, Effects of Grit Roughness and Pitch Oscillations on the S809 Airfoil. NREL/TP-442-7817, National Renewable Energy Laboratory, 1995.
 Leishman, J.G., Principles of Helicopter Aerodynamics. 2006.: Cambridge University Press.
 Rival, D. and C. Tropea, Characteristics of pitching and plunging airfoils under dynamic-stall conditions. J. Aircr. 47, (2010): p. 80–86.
 S.J. Schreck, Unsteady Vortex Dynamics and Surface Pressure Topologies on a Finite Pitching Wing. 1994., DTIC Document.