بررسی رفتار آیروالاستیک غیرخطی هواپیمای انعطاف‌پذیر کامل با روش مودهای فرضی و مدل آیرودینامیک حداقل متغیر فضای حالت

 [1] A. H. Nayfeh, Linear and nonlinear structural mechanics. John Wiley & Sons, (2024).

 [2] P. F. Pai, A. H. Nayfeh, Three-dimensional nonlinear vibrations of composite beams—I. Equations of motion. Nonlinear Dynamics, 1(6) (1990), 477-502.

 [3] C. da Silva, C. C. Glynn, Nonlinear flexural-flexural-torsional dynamics of inextensional beams. I. Equations of motion. Journal of Structural Mechanics, (1978) 6(4), 437-448.

 [4] D. H. Hodges, E. H. Dowell, Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades (1974) No. A-5711.

 [5] M. J. Patil, D. H. Hodges, C.E. Cesnik, Limit-cycle oscillations in high-aspect-ratio wings. Journal of fluids and structures, 15(1) (2001) 107-132.

 [6] T. Strganac, P. Cizmas, C. Nichkawde, J. Gargoloff, P. Beran, Aeroelastic analysis for future air vehicle concepts using a fully nonlinear methodology, In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, (2005) 2171.

 [7] M. H. Sadr Lahidjani, H. Haddadpour, S. Shams, Nonlinear aeroelastic behavior of a high flexibility wing with long span considering large deflection. In 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, (2004) 1943.

 [8] S. Shams, M. S. Lahidjani, H. Haddadpour, Nonlinear aeroelastic response of slender wings based on Wagner function. Thin-Walled Structures, 46 (11) (2008) 1192-1203.

[9] L. Meirovitch, and I. Tuzcu, Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft-Part I: System Modeling, AIAA Guidance, Navigation, and Control Conference and Exhibit, (2002) 4747.

[10] L. Meirovitch and I. Tuzcu, Integrated Approach to Flight Dynamics and Aeroservoelasticity of Whole Flexible Aircraft-Part I: System Modeling, AIAA Guidance, Navigation, and Control Conference and Exhibit, (2002)4747.

 [11] N. Nhan, and I. Tuzcu, Flight dynamics of flexible aircraft with aeroelastic and inertial force interactions.” AIAA atmospheric flight mechanics conference, 208 (2009) 109375.

 [12] I. Tuzcu, N. T. Nguyen, Modelling Dynamics of Highly Flexible Aircraft Using a Geometrically Nonlinear Structural Model, In AIAA SCITECH (2025) 1020.

 [13] M. R. Waszak, J. B. Davidson, D. K. Schmidt, A simulation study of the flight dynamics of elastic aircraft. Volume 1: Experiment, results and analysis, (1987) No. NASA-CR-4102.

 [14] D. K. Schmidt, B. P. Danowsky, A. Kotikalpudi, J. Theis, C.D. Regan, P. J. Seiler, R.K. Kapania, Modeling, design, and flight testing of three flutter controllers for a flying-wing drone. Journal of Aircraft, 57(4) (2020) 615-634.

 [15] C. Reschke, Integrated flight loads modelling and analysis for flexible transport aircraft, (2006).

 [16] L.T. Niblett, The fundamentals of body-freedom flutter, The Aeronautical Journal, 90(899) (1986) 373-377.

 [17] P. Shi, J. Liu, Y. Gu, Z. Yang, P. Marzocca, Full-span flying wing wind tunnel test: a body freedom flutter study. Fluids, 5(1) (2020) 34.

 [18] P. W. Richards, Y. Yao, R. A. Herd, D.H. Hodges, P. Mardanpour, Effect of inertial and constitutive properties on body-freedom flutter for flying wings. Journal of Aircraft, 53(3) (2016) 756-767.

 [19] A. Iannelli, A. Marcos, M. Lowenberg, Study of flexible aircraft body freedom flutter with robustness tools, Journal of Guidance, Control, and Dynamics 41(5) (2018) 1083-1094.

 [20] Y. D. Li, X. P. Zhang, Y. S. Gu, Z. C. Yang, Body freedom flutter study and passive flutter suppression for a high aspect ratio flying wing model. Applied Mechanics and Materials, 608 (2014) 708-712.

 [21] M. J. Patil, M. J. Nonlinear aeroelastic analysis, flight dynamics, and control of a complete aircraft. Georgia Institute of Technology (1999).

 [22] P. Mardanpour, D. H. Hodges, R. Neuhart, and N. Graybeal, Engine placement effect on nonlinear trim and stability of flying wing aircraft, Journal of Aircraft 50(6) (2013) 1716-1725.

 [23] I. Tuzcu, N.T. Nguyen, Modelling Dynamics of Highly Flexible Aircraft Using a Geometrically Nonlinear Structural Model. In AIAA SCITECH 2025 Forum, (2025) 1020.

[24] A. C. Gray, C. Riso, E. Jonsson, J.R. Martins, C. E. Cesnik, High-fidelity aerostructural optimization with a geometrically nonlinear flutter constraint. AIAA Journal, 61(6) (2023) 2430-2443.

[25] D. Sanghi, D., C. Riso, E. Cesnik, C. E., F. Vetrano, Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft. Journal of Aircraft, 2025.

 [26] J. Murua, R. Palacios, J. M. R. Graham, Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics. Progress in Aerospace Sciences, 55 (2012) 46-72.

 [27] Cheng, C. Wing, A. Cea, R. Palacios, A. Castrichini, and T. Wilson, Nonlinear Multibody Modelling of Flexible Aircraft with Flared Hinged Wings, In AIAA Scitech 2024 Forum, 2024, 1441.

 [28] D. K. Schmidt, B. P. Danowsky, A. Kotikalpudi, J. Theis, C.D. Regan, P. J. Seiler, R. K. Kapania, Modeling, design, and flight testing of three flutter controllers for a flying-wing drone. Journal of Aircraft, 57(4) (2020) 615-634.

[29] S. Shafaghat, M. A. Noorian, S. Irani, Nonlinear aeroelastic analysis of a HALE aircraft with flexible components, Aerospace Science and Technology 127 (2022) 107663.

[30] S. Shafaghat, M. Noorian, S. Irani, Nonlinear body-freedom flutter analysis in aircraft with the flexible wing, Aerospace Knowledge and Technology Journal, (2022) 191-204.

[31] S. Shafaghat, M. A. Noorian, Modeling and Analysis of Aeroelastic Instabilities in a Flexible Full Aircraft Using Quasi-Coordinate Formulation and Minimum State Aerodynamic Model. Amirkabir Journal of Mechanical Engineering, (2025).

 [32] M. Karpel, Design for active and passive flutter suppression and gust alleviation, Stanford University, (1980).

 [33] J. Eirikur, C. Riso, C. A. Lupp, C. Cesnik, J. Martins, and B. Epureanu, Flutter and post-flutter constraints in aircraft design optimization, Progress in Aerospace Sciences 109 (2019) 100537.

 [34] M. Nejati, S. Shokrollahi, S. Shams, Nonlinear aeroelastic analysis of high-aspect-ratio wings using indicial aerodynamics. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 40(6) (2018) 298.