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ORIGINAL PAPER
Bending vibrations of a thin wing for a profile with two axes of symmetry
1
Department of Mathematics, Faculty of Applied Sciences, Ho Chi Minh City University of Technology and Education, Ho Chi Minh City, Vietnam, Viet Nam
These authors had equal contribution to this work
Submission date: 2024-06-13
Final revision date: 2024-09-17
Acceptance date: 2024-10-18
Online publication date: 2024-12-12
Publication date: 2024-12-12
Corresponding author
Thanh Thi Le
Department of Mathematics, Faculty of Applied Sciences, Ho Chi Minh City University of Technology and Education, Ho Chi Minh City, Vietnam, Viet Nam
Department of Mathematics, Faculty of Applied Sciences, Ho Chi Minh City University of Technology and Education, Ho Chi Minh City, Vietnam, Viet Nam
International Journal of Applied Mechanics and Engineering 2024;29(4):106-120
KEYWORDS
natural frequenciesMach numbertorsional vibrationsbending vibrationsairfoil with two axes of symmetry
TOPICS
ABSTRACT
In this work, we study the bending vibrations of a thin wing for a profile with two axes of symmetry, taking into account the influence of torsional vibrations on them. The primary focus of the current study is on finding an analytic solution for the wing-bending equation through the Laplace transform, determining the frequency of free-bending vibrations, and constructing the amplitude-frequency response and phase-frequency response of the wing.
REFERENCES (19)
1.
Thanh L.T. (2023): Determination of the critical velocity of a straight wing with a high aspect ratio.– International Journal of Applied Mechanics and Engineering, vol.28, No.1, pp.105-117, https://doi.org/10.59441/ijame....
2.
Volmir A.S. (1972): Nonlinear Dynamics of Plates and Shells.– Moscow, Science, p.432.
3.
Volmir A.S. (1976): Shells in Liquid and Gas Flow: Problems of Aeroelasticity.– Moscow, Science, p.416.
5.
Fyn Ya. Ts. (1959): Introduction to The Theory of Aero-stiffness.– Moscow, State Publishing House of Physical and Mathematical Literature, p. 522.
6.
Vedeneev V.V. (2005): Flutter of a broad stripe-shaped plate in a supersonic gas flow.– News of the Russian Academy of Sciences, Mechanics of liquid and gas. No.5. pp. 155-169.
7.
Bolotin V.V. (1961): Non-conservative Problems of The Theory of Elastic Stability.– Moscow, State Publishing House of Physical and Mathematical Literature, p.338.
8.
Demidovich B.P. (1967): Lectures on The Mathematical Theory of Stability.– Moscow, Nauka, p.532.
9.
Seher Eken (2019): Free vibration analysis of composite aircraft wings modelled as thin-walled beams with NACA airfoil sections.– Thin-Walled Structures, vol.139, pp.362-377, https://doi.org/10.1016/j.tws.....
10.
Pranjal Agrawal, Pankaj Dhatrak, Paras Choudhary (2021): Comparative study on vibration characteristics of aircraft wings using finite element method.– Materials Today: Proceedings, vol.46, part1, pp.176-183, https://doi.org/10.1016/j.matp....
11.
Zhou Z. (2023): Vibration analysis of airplane wing under fuel weight.– In: Yadav S., Kumar H., Wan M., Arora P.K., Yusof Y., (eds) Recent Advances in Applied Mechanics and Mechanical Engineering. ICAMME 2022. Lecture Notes in Mechanical Engineering. Springer, Singapore, pp.459-468, https://doi.org/10.1007/978-98....
12.
Evran S., Kurt M., and Kurt A. (2020): Evaluation of cross-section and wing length in free vibration analysis of aircraft wings.– Journal of Aviation, vol.4, No.2, pp.17-24, https://doi.org/10.30518/jav.7....
13.
Maamo M.S., Afonin A.A. and Sulakov A.S. (2022): Aircraft wing vibration parameters measurement system using MEMS IMUs and closed-loop optimal correction.– Aerospace Systems, vol.5, pp.473-480, https://doi.org/10.1007/s42401....
14.
Zverev A.Y. and Chernyh V.V. (2022): Promising methods for reducing the vibrations of aircraft structures under acoustic excitation.– Dokl. Phys. vol.67, pp.369-376, https://doi.org/10.1134/S10283....
15.
Guo Yao, Mingjun Song, Lisha Zhu (2023): Time-varying stability and vibration of an embedded thin plate on a swept wing.– Aerospace Science and Technology, vol.140, p.108436, https://doi.org/10.1016/j.ast.....
16.
Gryazev M.V., Zheltkov V.I., Vasin A.A. and Vasina M.V. (2011): Applied problems in the mechanics of a deformable solid.– Statics of Rods. Tula State University Publishing House, part 1, p.112.
17.
Ilyushin A.A. and Pobedrya B.E. (1970): Fundamentals of The Mathematical Theory of Thermo Viscoelasticity.– Moscow, Nauka, p.238.
18.
Kholodov A.A. (2009): Determination of damping characteristics of steel grade steel 3.– Fundamental and Applied Problems of Engineering and Technology, No.5, pp.12-17.
19.
Iorish Yu.I. (1963): Vibrometry.– Moscow, State Scientific and Technical Publishing House of Mechanical Engineering Literature, p.756.
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