D. Thompson, J. Feys, M. Filewich, S. Abdel-Magid, D. Dalli, and F. Goto, The design and construction of a blended wing body UAV,in 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, pp. 481, 2011.
 K. M. Bieri, An Integrated Bi-Fidelity Approach to Parametric Studies of Finite Wing Geometries, University of Colorado at Boulder, 2019.
 H. Dastourani, MH. Djavareshkian, Aerodynamic investigation of potential flow on integrated wing and body aircraft, Modeling in engineering, vol. 14, No. 47, pp. 127-140, 2017. )in Persian ).
 L. Peifeng, B. Zhang, C. Yingchun, Y. Changsheng, and L. Yu, Aerodynamic design methodology for blended wing body transport, Chinese Journal of Aeronautics, vol. 25, No. 4, pp. 508-516, 2012.
 G. Stenfelt and U. Ringertz, Yaw control of a tailless aircraft configuration, Journal of aircraft, vol. 47, No. 5, pp. 1807-1811, 2010.
 M. Dehghan Menshadi, M.Il Begi, Mehrdad Bezazzadeh, Mohammad Kazem Sobhani, Experimental investigation of the vortex flow of a lambda-shaped wing sample with a sharp and rounded leading edge with a hot wire, mechanical engineering, vol. 32, No. 1, pp. 107-117, 2016.) in Persian ).
 A. LEVY, M. KATZ, O. KATZUNI, A. KONEVSKY, J. FRUMKIN, and T. BUIUM, Final Report Project 7-8: Team Cerberus-UCAV, Haifa, Israel, 2009
 R. Konrath, E. Roosenboom, A. Schröder, D. Pallek, and D. Otter, "Static and dynamic SACCON PIV tests, part II: aft flow field," in 28th AIAA applied aerodynamics conference, p. 4396, 2010.
 K. Petterson, Low-speed aerodynamic and flowfield characteristics of a UCAV, in 24th AIAA Applied Aerodynamics Conference, pp. 2986, 2006.
 A. Ko, K. Chang, D.-J. Sheen, Y.-H. Jo, and H. J. Shim, "CFD Analysis of the Sideslip Angle Effect around a BWB Type Configuration," International Journal of Aerospace Engineering, vol. 2019, 2019.
 M. Ramezanizadeh and A. Mohammadi, Numerical Investigation of Delta Wings Leading Edge Configuration Effects on the Flow Behavior Using Large Eddy Simulation Approach, Journal of Aeronautical Engineering,Vol.3, No.3,2014.( in Persian )
 N. U. Rahman and J. F. Whidborne, Propulsion and flight controls integration for a blended-wing-body transport aircraft, Journal of Aircraft, vol. 47, No. 3, pp. 895-903, 2010.
 R. Colgren and R. Loschke, "Effective design of highly maneuverable tailless aircraft," Journal of Aircraft, vol. 45, no. 4, pp. 1441-1449, 2008.
 Z. J. Li and D. L. Ma, Control characteristics analysis of split-drag-rudder, in Applied Mechanics and Materials,vol. 472, pp. 185-190, 2014.
 P. Bourdin, A. Gatto, and M. Friswell, Potential of articulated split wingtips for morphing-based control of a flying wing, in 25th AIAA Applied Aerodynamics Conference, p. 4443, 2007.
 D. Li, Q. Liu, Y. Wu, and J. Xiang, Design and analysis of a morphing drag rudder on the aerodynamics, structural deformation, and the required actuating moment, Journal of Intelligent Material Systems and Structures, vol. 29, No. 6, pp. 1038-1049, 2018.
 A. Madani and M. H. Djavareshkian, Aerodynamic Investigation of Crow Flap Control System in a Flying Wing UAV Aircraft, Journal of Aeronautical Engineering, 2022.( in Persian )
 G. Stenfelt and U. Ringertz, Lateral stability and control of a tailless aircraft configuration, Journal of Aircraft, vol. 46, No. 6, pp. 2161-2164, 2009.
 J. Rajput, W. G. Zhang, and X. B. Qu, A differential configuration of split drag-rudders with variable bias for directional control of flying-wing,in Applied Mechanics and Materials, vol. 643 , pp. 54-59, 2014.
 A. Madani, M. H. Djavareshkian, and R. Karimi Kelayeh, Optimization of split drag rudder mechanism at different angles of attack in a flying wing airplane,Fluid Mechanics & Aerodynamics Journal, vol. 11, No. 1, pp. 1-16, 2022.( in Persian )
 N. U. Rahman and J. F. Whidborne, A lateral directional flight control system for the MOB Blended Wing Body planform, in Proceedings of the UK ACC International Conference on Control, Manchester, UK, pp. 2 4,2008.
 R. K. Kelayeh and M. H. Djavareshkian, "Aerodynamic investigation of twist angle variation based on wing smarting for a flying wing," Chinese Journal of Aeronautics, vol. 34, No. 2, pp. 201-216, 2021.
 M. Tomac and G. Stenfelt, Predictions of stability and control for a flying wing, Aerospace Science and Technology, vol. 39, pp. 179-186, 2014.