Effect of Magnetic Field on Aeroelastic Stability of High Aspect Ratio Plate

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This paper studies how a magnetic field affects the stability domain of a high aspect-ratio plate subjected simultaneously to supersonic gas flow and a temperature gradient across its thickness. Formulating the problem mathematically leads to a boundary value problem describing the plate’s stable configuration. The model is built on the fundamental assumptions of magneto-thermo-elastic plate theory and piston theory. It also employs an extended formula of piston theory, previously derived and explained in detail in [1,2]. Using the Routh–Hurwitz criterion, the study determines the stability regions of the plate under the combined effects of the temperature field and the external flow, and analyzes how the magnetic field modifies these regions. Additionally, based on an obtained formula for the critical flow velocity, the paper computes the corresponding critical velocities for various temperature distributions and explores the impact of the magnetic field on these values.

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3-15

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August 2026

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[1] Baghdasaryan G.Y., Mikilyan M.A. Magnetoelastic Vibrations and Stability of Magnetically Active Plates and Shells. Springer, 2024.

DOI: 10.1007/978-3-031-60307-5

Google Scholar

[2] Mikilyan M.A., Vardanyan I.A. The effects of magnetic field on supersonic flutter characteristics of dielectric plate: Dependence amplitude-speed. Journal of Fluids and Structures, 2024, vol. 128, 104140.

DOI: 10.1016/j.jfluidstructs.2024.104140

Google Scholar

[3] Baghdasaryan G., Mikilyan M., Saghoyan R., Cestino E. Frulla G., Marzocca P. Nonlinear LCO "amplitude–frequency" characteristics for plates fluttering at supersonic speeds. International Journal of Non-Linear Mechanics, Volume 77, December 2015, Pages 51–60.

DOI: 10.1016/j.ijnonlinmec.2015.06.014

Google Scholar

[4] Bolotin V.V. Non-conservative problems of the theory of elastic stability. – Moscow, Fizmatgiz, 1961. -339 p.

Google Scholar

[5] Miles J. W., Supersonic flutter of a cylindrical shell, Journal of Aeronautical Science Vol. 24, No. 2, 1957; Vol. 25, No. 5, 1958, pp.107-118.

DOI: 10.2514/8.3780

Google Scholar

[6] Dowell. E.H. "Nonlinear oscillations of a fluttering plate." AIAA Journal, Vol. 4, No. 7, 1966, pp.1267-1275.

DOI: 10.2514/3.3658

Google Scholar

[7] Dowell. E.H. "Nonlinear oscillations of a fluttering plate. II." AIAA Journal, Vol. 5, No. 10, 1967, pp.1856-1862.

DOI: 10.2514/3.4316

Google Scholar

[8] Miles J. W., Supersonic flutter of a cylindrical shell, Journal of Aeronautical Science Vol. 24, No. 2, 1957; Vol. 25, No. 5, 1958, pp.107-118.

DOI: 10.2514/8.3780

Google Scholar

[9] Baghdasaryan G., Mikilyan M., Vardanyan I., Danoyan E.H., Melikyan K. Influence of boundary conditions on the aero-thermo-elastic stability of a closed cylindrical shell. IOP Conf. Series: Journal of Physics: Conf. Series 1474 (2020) 012008;.

DOI: 10.1088/1742-6596/1474/1/012008

Google Scholar

[10] Baghdasaryan G., Mikilyan M., Vardanyan I., Melikyan K.V., Marzocca P. Thermoelastic non-linear flutter oscillations of rectangular plate. Journal of Thermal stresses, 2021, vol.44(6), pp.731-754.

DOI: 10.1080/01495739.2021.1914528

Google Scholar

[11] Baghdasaryan G., Mikilyan M., Vardanyan I., Panteleev A., Severina N.S. Nonlinear flutter responce of cylindrical shell in thermal field and supersonic gas flow. IOP Conf. Series: Materials Science and Engineering, 2020, 927(1), 012022;.

DOI: 10.1088/1757-899X/927/1/012022

Google Scholar

[12] Mikilyan M.A. Thermoelastic Response of Closed Cylindrical Shells in a Supersonic Gas Flow. Aerospace 2020, 7(8), 103;.

DOI: 10.3390/aerospace7080103

Google Scholar

[13] Baghdasaryan G.Y., Mikilyan M.A., Marzocca, P. Supersonic flutter characteristics of dielectric rectangular plate: The effects of magneto-aero-hydrodynamic interactions. Journal of Fluids and Structures, 2023, 118, 103856.

DOI: 10.1016/j.jfluidstructs.2023.103856

Google Scholar

[14] Borghi C.A., Carraro M.R., and Cristofolini A., "Analysis of Magnetoplasmadynamic Interaction in the Boundary Layer of a Hypersonic Vehicle", Journal of Spacecraft and Rockets, Vol. 41, No. 4, 2004.

DOI: 10.2514/1.4031

Google Scholar

[15] Borghi C.A., Carraro M.R., and Cristofolini A., "Magnetohydrodynamics Interaction in the Shock Layer of a Wedge in a Hypersonic Flow", IEEE Transaction on Plasma Science, vol. 34, no. 5, October 2006.

DOI: 10.1109/tps.2006.883377

Google Scholar

[16] Cristofolini A. et al., "Experimental Investigation on the MHD Interaction around a Sharp Cone in an Ionized Argon Flow", AIAA-2006-3075, 37th AIAA Plasmadynamics and Lasers Conference, San Francisco, California, June 2006.

DOI: 10.2514/6.2006-3075

Google Scholar

[17] Mikilyan M.A. Nature of Supersonic Flutter of Aero-Magneto-Elastic System at Pre-Critical Flowing Speeds. IEEE Aerospace Conference Proceedings, 2024, pp.529-537.

DOI: 10.1109/aero58975.2024.10521224

Google Scholar

[18] Bagdasaryan G., Mikilyan M. Effects of Magnetoelastic Interactions in Conductive Plates and Shells. Springer, 2016, -286p.

Google Scholar

[19] Bolotin V.V. Non-conservative problems of the theory of elastic stability. – Moscow, Fizmatgiz, 1961. -339 p.

Google Scholar

[20] Vlasov V. Z. The General Theory of Shells, Gostekhizdat, Moscow, 1949.

Google Scholar

[21] Volmir S. Non-linear Dynamics of Plates and Shells, Nauka, Moscow, 1972.

Google Scholar

[22] Chhunchha A., Samra H.S., Divye S. Applied magneto-aerodynamics for safer re-entry of space vehicle. 64th International Astronautical Congress, Beijing, China, 2013, by the International Astronautical Federation.

Google Scholar