[1] J. Zhang, J. Lei, J. Niu, Numerical investigation of aerodynamic characteristics of free-spinning tail projectile with canards roll control, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 235(6) (2021) 687-702.
[2] B.B. Gloss, L.W. Mckinney, Canard-wing lift interference related to maneuvering aircraft at subsonic speeds, (1973).
[3] B.B. Gloss, The effect of canard leading edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristic of a close-coupled canard-wing configuration, (1974).
[4] B.B. Gloss, Effect of Canard Location and Size on Canard-Wing Interference and Aerodynamic-Center Shift Related to Maneuvering Aircraft at Transonic Speeds. NASA Report, 1974, NASA TN D-7505, (1974).
[5] H.-C. Oelker, D. Hummel, Investigations on the vorticity sheets of a close-coupled delta-canard configuration, Journal of aircraft, 26(7) (1989) 657-666.
[6] D. Hummel, H.C. Oelker, Effects of canard position on the aerodynamic characteristics of a close-coupled canard configuration at low speed, Zeitschrift für Flugwissenschaften und Weltraumforschung, 15(2) (1991) 74-88.
[7] Z. Lu, Z. Lu, A study on flow patterns and aerodynamic characteristics for canard-double delta wing configuration, in: 35th Aerospace Sciences Meeting and Exhibit, 1994, pp. 324.
[8] S. Hayashibara, R. Myose, L. Miller, The effect of a 70 swept canard-on the leading edge vortices of a 70 swept delta wing during dynamic pitching, AIAA Paper 97, 613 (1997).
[9] V.J. Stark, Canard-wing interaction in unsteady supersonic flow, Journal of aircraft, 26(10) (1989) 951-952.
[10] S.K. Hebbar, M.F. Platzer, D.-M. Liu, Effect of canard oscillations on an X-31A-like model in pitching maneuver, Journal of aircraft, 32(5) (1995) 1157-1160.
[11] Q. Chen, T. Hu, P. Liu, Q. Qu, H. Guo, R.A. Akkermans, The dynamic vortical flow behaviour on a coplanar canard configuration during large-amplitude-pitching, Aerospace Science and Technology, 112 (2021) 106553.
[12] S.M. Hitzel, R. Osterhuber, Enhanced maneuverability of a delta-canard combat aircraft by vortex flow control, Journal of Aircraft, 55(3) (2018) 1090-1102.
[13] J. Sahu, F. Fresconi, Computational and Experimental Free-Flight Motion of a Subsonic Canard-Controlled Body, in: 35th AIAA Applied Aerodynamics Conference, 2017, pp. 3400.
[14] S.B. Wibowo, S. Sutrisno, T.A. Rohmat, Computational study of flow interactions over a close coupled canard-wing on fighter, International Journal of Aviation, Aeronautics, and Aerospace, 6(1) (2019) 5.
[15] K.V.R.A.N.K.P.B.S.T. Sudhakar Uppalapati, CFD Analysis on Eurofighter Typhoon at Canard, International Journal of Advanced Science and Technology, 29(9s) (2020) 2408 - 2415.
[16] D. Hummel, G. Redeker, A new vortex flow experiment for computer code validation, NATO RESEARCH AND TECHNOLOGY ORGANIZATION NEUILLY-SUR-SEINE (FRANCE), 2003.
[17] D.J. Hummel, The international vortex flow experiment 2 (VFE-2): background, objectives and organization, Aerospace science and technology, 24(1) (2013) 1-9.
[18] J.M. Luckring, D. Hummel, What was learned from the new VFE-2 experiments, Aerospace Science and Technology, 24(1) (2013) 77-88.
[19] M. Hadidoolabi, H. Ansarian, Computational investigation of vortex structure and breakdown over a delta wing at supersonic pitching maneuver, Journal of the Brazilian Society of Mechanical Sciences and Engineering, 40(2) (2018) 1-17.
[20] S.B. Wibowo, B. Basuki, T.A. Rohmat, S. Siswantoro, F. Nugroho, P. Ginting, Z. Anwar, Vortex Dynamics Study and Flow Visualization on Aircraft Model with Different Canard Configurations, Fluids, 6(4) (2021) 144.
[21] Y. Dong, Z. Shi, K. Chen, J. Chen, Experimental investigation of the effects of sideslip on canard-configuration aircraft at high angle of attack, AIP Advances, 9(5) (2019) 055114.
[22] Z. Ali, W. Kuntjoro, W. Wisnoe, I. Ishak, M. Katon, N. Ahmad, Aerodynamics Analysis on the Effect of Canard Aspect Ratio on Blended Wing Body Aircraft using CFD Simulation, in: IOP Conference Series: Materials Science and Engineering, IOP Publishing, 2020, pp. 012015.
[23] M. Soltani, F. Askari, A. Davari, A. Nayebzadeh, Effects of canard position on wing surface pressure, (2010).
[24] M.H. Doolabi and M.A. Rabbani, Numerical investigation of the flowfield over a closely coupled canard-wing configuration in subsonic flow. The 26th annual conference of the Iranian Society of Mechanical Engineers (ISME 2018), Semnan University, Iran 24-26 April, (2018).
[25] A.R. Davari, M.H. Doolabi, M. Soltani, M. Izadkhah, Aspects of canard-wing vortices interaction in subsonic flow, Scientia Iranica, 22(3) (2015) 743-754.
[26] M. Hadidoolabi, H. Ansarian, Computational Investigation of Vortex Breakdown over a Pitching Delta Wing at Supersonic Speeds, Scientia Iranica, 24(6) (2017) 2915-2928.