Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model-Reference-Cited by-同舟云学术

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Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model

Published:2021-06-28 Issue:9 Volume:232 Page:3539-3564
ISSN:0001-5970
Container-title:Acta Mechanica
language:en
Short-container-title:Acta Mech

Author:

Ye Liuqing,Ye Zhengyin,Ye Kun,Wu Jie

Funder

National Natural Science Foundation of China

National Numerical Wind-tunnel

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Link

https://link.springer.com/content/pdf/10.1007/s00707-021-03023-3.pdf

Reference45 articles.

1. Dowell, E.H.: Nonlinear oscillations of a fluttering plate. AIAA J. 4(7), 1267–1275 (1966). https://doi.org/10.2514/3.3658

2. Dowell, E.H.: Nonlinear oscillations of a fluttering plate. II. AIAA J. 5(10), 1856–1862 (1967). https://doi.org/10.2514/3.4316

3. Wang, X.C., Yang, Z.C., Chen, Z.L., Gu, Y.S., Wang, W.Q., Zhao, Y., Wang, Y.M.: Study on coupled modes panel flutter stability using an energy method. J. Sound Vib. 468, 1–16 (2020). https://doi.org/10.1016/j.jsv.2019.115051

4. Aditya, S., Haboussi, M., Shubhendu, S., Ganapathi, M., Polit, O.: Supersonic flutter study of porous 2D curved panels reinforced with graphene platelets using an accurate shear deformation finite element procedure. Compos. Struct. 241, 1–11 (2020). https://doi.org/10.1016/j.compstruct.2020.112058

5. Muc, A., Flis, J.: Free vibrations and supersonic flutter of multilayered laminated cylindrical panels. Compos. Struct. 246, 1–10 (2020). https://doi.org/10.1016/j.compstruct.2020.112400

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1. Prediction of SBLI Induced Flexible Panel Motion using Wall-Modeled LES Coupled to an Aeroelastic Solver;AIAA SCITECH 2024 Forum;2024-01-04

2. Numerical study on the nonlinear characteristics of shock induced two-dimensional panel flutter in inviscid flow;Journal of Sound and Vibration;2023-11

3. Numerical study on the nonlinear characteristics of shock induced two-dimensional panel flutter in inviscid flow;2022-09-30

4. Effect of Micro-Vortex Generator on Panel Flutter in Shock Wave-Boundary Layer Interaction;AIAA AVIATION 2022 Forum;2022-06-20

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