[1] Mattos, B.S.D. and Secco, N.R., An airplane calculator featuring a high-fidelity methodology for tailplane sizing, Journal of Aerospace Technology and Management, Vol. 5, pp.371-386, 2013.
[2] Sadraey, M.H., Aircraft design: A systems engineering approach, John Wiley & Sons,. 2012.
[3] Nicolosi, F., Ciliberti, D., Della Vecchia, P., Corcione, S. and Cusati, V., A comprehensive review of vertical tail design, Aircraft Engineering and Aerospace Technology, Vol. 89, No. 4, pp.547-557, 2017.
[4]https://en.wikipedia.org/wiki/Vertical_stabilizer.
[5] Whalen, E.A., Shmilovich, A., Spoor, M., Tran, J., Vijgen, P., Lin, J.C. and Andino, M., Flight test of an active flow control enhanced vertical tail, AIAA Journal, Vol. 56, No. 9, pp.3393-3398, 2018.
[6] Zachos, P.K., Modelling and analysis of turbofan engines under windmilling conditions, Journal of Propulsion and Power, Vol. 29, No. 4, pp.882-890, 2013.
[7] Götz, V.G., Windmilling in aero-engines, Doctoral dissertation, Ph. D. thesis, University of London, Imperial College of Science, Technology and Medicine, Kensington, UK, 2001.
[8] Whalen, E.A., Spoor, M., Vijgen, P.M., Tran, J., Shmilovich, A., Lin, J.C. and Andino, M., Full-scale flight demonstration of an active flow control enhanced vertical tail, In 8th AIAA Flow Control Conference, pp. 3927, 2016.
[9] Shams Taleghani, A., Ghajar, A. and Masdari, M., Experimental Study of Ground Effect on Horizontal Tail Effectiveness of a Conceptual Advanced Jet Trainer, Journal of Aerospace Engineering, vol. 33, no. 4, p. 05020001, 2020.
[10] Scholz, P., Singh, V.M., Gebhardt, A., Löffler, S. and Weiss, J., The efficiency of different flow control methods on a vertical tail, In AIAA Scitech 2020 Forum, pp. 1537, 2020.
[11] Raymer, D., Aircraft design: A conceptual approach, 5th ed., American Institute of Aeronautics and Astronautics,Inc., 2012.
[12] Hettema, A.P., Vertical Tail Design: Development of a rapid aerodynamic analysis method, Master of Science in Aerospace Engineering, Delft University of Technology, 2015.
[13] Torenbeek, E., Synthesis of subsonic airplane design: an introduction to the preliminary design of subsonic general aviation and transport aircraft, with emphasis on layout, aerodynamic design, propulsion and performance. Springer Science & Business Media, 2013.
[14] Roskam, J., Airplane design, Part III: Layout design of cockpit, fuselage, wing and empennage: Cutaways and inboard profiles, 1st ed., Roskam Aviation and Engineering Corporation, 1986.
[15] Le, L.D., Preliminary design of commercial aircraft from the academic perspective, Master of science thesis, University of Minnesota, 2012.
[16] Andino, M.Y., Lin, J.C., Roman, S., Graff, E.C., Gharib, M., Whalen, E.A. and Wygnanski, I.J., Active flow control on vertical tail models, AIAA Journal, Vol. 57, No. 8, pp. 3322-3338, 2019.
[17] Ciliberti, D., Nicolosi, F., and Della Vecchia, P., A new approach in aircraft vertical tailplane design, In 22th AIDAA Conference, Associazione Italiana di Aeronautica e Astronautica Naples (Italy), September 2013.
[18] Ciliberti, D., Della Vecchia, P., Nicolosi, F., and De Marco, A., Aircraft directional stability and vertical tail design: A review of semi-empirical methods, Progress in Aerospace Sciences, Vol. 95, pp. 140-172, 2017.
[19] Jenkinson, L.R., Simpkin, P., Rhodes, D., Jenkison, L.R., and Royce, R., Civil jet aircraft design, Vol. 338, London, UK: Arnold, 1999.
[20] Kundu, A.K., Aircraft design, Vol. 27, Cambridge University Press, 2010.
[21] Ciliberti, D., A new vertical tailplane design procedure through CFD, Doctoral dissertation, Master thesis in Aerospace Engineering, Department of Aerospace Engineering, University of Naples Federico II, 2012.
[22] Ciliberti, D., An improved preliminary design methodology for aircraft directional stability prediction and vertical tailplane sizing, Doctoral Thesis, University of Naples Federico II, 2016.
[23] Lin, J.C., Whalen, E.A., Andino, M.Y., Graff, E.C., Lacy, D.S., Washburn, A.E., Gharib, M., and Wygnanski, I.J., Full-scale testing of active flow control applied to a vertical tail, Journal of Aircraft, Vol. 56, No. 4, pp.1376-1386, 2019.
[24] Nicolosi, F., Ciliberti, D., Della Vecchia, P. and Corcione, S., Experimental analysis of aircraft directional control effectiveness, Aerospace Science and Technology, Vol. 106, pp.106099, 2020.
[25] De Wit, A.J., Lammen, W.F., Vankan, W.J., Timmermans, H., Van Der Laan, T. and Ciampa, P.D., Aircraft rudder optimization-A multi-level and knowledge-enabled approach, Progress in Aerospace Sciences, Vol. 119, pp.100650, 2020.
[26] Abdolahipour, S., Mani, M., and Ahmadi Dehaghi, G. M., Numerical and Experimental Study of the Influence of Damage on the Aerodynamic Characteristics of a Finite Wing. Fluids Engineering Division Summer Meeting, vol. 44403, pp. 1441-1447, 2011.
[27] Izadi, M., Khaki, R., Shams Taleghani, A., Ghajar, A., A study of the effects of smart flap on model airfoil of fighter, journal of aeronautical engineering, Vol. 22, Issue 2, pp. 80-97, 2020. (in Persianفارسی )
[28] Fallahian, a., Shams Taleghani, A., Esmailpour, K., Three-Dimensional Numerical Study of the Effect of Blowing Angle on the Aerodynamic Characteristics of a Wing Section with NACA 0012 Airfoil, Aerospace Knowledge and Technology Journal, 12, 1, 2023. (in Persianفارسی )
[29] Abdizadeh, g., Ghasemloo, s., Improve aerodynamic coefficients on dynamic stall oscillating airfoil by using Plasma Actuator, Aerospace Knowledge and Technology Journal, 10, 1, 2021. (in Persianفارسی )
[30] Parhizkar, H., Numerical Simulation of Flow Past Oscillating Airfoil Using Oscillation of Flow Boundary Condition, Journal of Aerospace Science and Technology, 3, 1, 2006. (in Persianفارسی )
[31] Abdolahipour, S., Mani, M., Shams Taleghani, A., Pressure Improvement on a Supercritical High-Lift Wing Using Simple and Modulated Pulse Jet Vortex Generator, Flow, Turbulence and Combustion, Vol. 109, pp. 65–100, 2022.
[32] Ahmadpour Roudsari, M., Parhizkar, H., Pouryoussefi, G.H., Tarabi, A., Numerical investigation of factors affecting in the steady and unsteady plasma actuators performance on the airflow through the flat plate, Modares Mechanical Engineering, 18, 1, 2018. (in Persianفارسی )
[33] Abdolahipour, S., Effects of Low and High Frequency Actuation on Aerodynamic Performance of a Supercritical Airfoil, Frontiers in Mechanical Engineering, Vol. 9, 2023. doi: 10.3389/fmech.2023.1290074
[34] Abdolahipour, S., Numerical investigation of the flow control by a pulsed vortex generator jet on the turbulent flow of an airfoil. Aerospace Knowledge and Technology Journal, Vol. 12, No. 2, pp.79-97, 2024.
[35] Abdolahipour, S., Mani, M., Shams Taleghani, A., Experimental Investigation of Flow Control on a High-Lift Wing Using Modulated Pulse Jet Vortex Generator, Journal of Aerospace Engineering, (ASCE) Vol. 35, Issue 5, 2022.
[36] Shmilovich, A.,Whalen, E.A., A technique for low input flow control actuation, In 35th AIAA Applied Aerodynamics Conference, pp. 3040, 2017.
[37] Rasquin, M., Farnsworth, J.A., Balin, R., Jansen, K.E., Modeling strategies of active flow control applied to a vertical tail assembly, In AIAA AVIATION 2020 FORUM, pp. 2944, 2020.
[38] Xu, K., Zha, G., High control authority 3d aircraft control surfaces using co-flow jet, In AIAA Aviation 2019 Forum, pp. 3168, 2019.
[39] Jansen, K.E., Rasquin, M., Farnsworth, J.A., Rathay, N., Monastero, M.C., Amitay, M., Interaction of a synthetic jet with separated flow over a vertical tail, AIAA Journal, 56, 7, pp. 2653-2668, 2018.
