Multi-objective optimization on thermomechanical behaviors of temperature-dependent graphene platelet reinforced sandwich plates DOI Creative Commons

Yushan Xiao,

Wu Zhen

Chinese Journal of Aeronautics, Год журнала: 2024, Номер unknown, С. 103363 - 103363

Опубликована: Дек. 1, 2024

Язык: Английский

Nonlinear aero-thermo-elastic flutter analysis of stiffened graphene platelets reinforced metal foams plates with initial geometric imperfection DOI
Jinpeng Song, Gui-Lin She, Mohamed A. Eltaher

и другие.

Aerospace Science and Technology, Год журнала: 2024, Номер 147, С. 109050 - 109050

Опубликована: Март 11, 2024

Язык: Английский

Процитировано

30

State-of-the-Art Review of Computational Static and Dynamic Behaviors of Small-Scaled Functionally Graded Multilayer Shallow Arch Structures from Design to Analysis DOI

Dogus Hurdoganoglu,

Babak Safaei, Saeid Sahmani

и другие.

Archives of Computational Methods in Engineering, Год журнала: 2023, Номер 31(1), С. 389 - 453

Опубликована: Авг. 14, 2023

Язык: Английский

Процитировано

20

Nonlinear dynamic analysis of the graphene platelets reinforced porous plate with magneto-electro-elastic sheets subjected to impact load DOI
Yuhang Tian, Qingya Li,

Yuan Feng

и другие.

Nonlinear Dynamics, Год журнала: 2023, Номер 112(3), С. 1661 - 1690

Опубликована: Дек. 19, 2023

Язык: Английский

Процитировано

12

Free vibration of FG multilayer hybrid nanocomposite microbeam reinforced by GPLs and CNTs under nonlocal dual-phase-lag generalized thermoelastic theory DOI
Xinfei Zhang, T.C. Wang, Peng Wei

и другие.

Archive of Applied Mechanics, Год журнала: 2024, Номер 94(10), С. 2819 - 2839

Опубликована: Июнь 27, 2024

Язык: Английский

Процитировано

3

Supersonic Dynamic Instability Of Imperfect FG-GPLRC Truncated Conical Shell Subjected To Follower Force, Internal Pressure And Thermal Effect DOI
Rupsagar Chatterjee, Sudib Kumar Mishra

Опубликована: Янв. 1, 2025

Язык: Английский

Процитировано

0

Influences of the graphene reinforcements on the natural vibrational properties, nonlinear flutter responses, and the chaotic motions of the FG-GR laminated composite cantilever rectangular variable cross-section plate in the supersonic flow DOI
Y. Jiang, Yu Wang, Wei Zhang

и другие.

Chaos Solitons & Fractals, Год журнала: 2025, Номер 194, С. 116221 - 116221

Опубликована: Фев. 28, 2025

Язык: Английский

Процитировано

0

An isogeometric approach to supersonic flutter analysis of lightweight-designed plates with graphene reinforcement DOI
Nam V. Nguyen,

Thoai N. Tran

Advances in Engineering Software, Год журнала: 2025, Номер 208, С. 103955 - 103955

Опубликована: Июнь 6, 2025

Язык: Английский

Процитировано

0

Nonlinear dynamics of nanocomposite beam-like aerospace structures DOI
Krzysztof Kamil Żur, Hassan Mohammadi, Y. Kiani

и другие.

Engineering Analysis with Boundary Elements, Год журнала: 2024, Номер 165, С. 105812 - 105812

Опубликована: Июнь 3, 2024

Язык: Английский

Процитировано

2

Semianalytical Research on Aerothermoelastic Behaviors of Functionally Graded Plates under Arbitrary Temperature Fields in Hypersonic Vehicles DOI Creative Commons
Chang Li, Zhiqiang Wan, Xiaozhe Wang

и другие.

Aerospace, Год журнала: 2024, Номер 11(7), С. 572 - 572

Опубликована: Июль 12, 2024

Hypersonic vehicles are susceptible to considerable aerodynamic heating and noticeable aerothermoelastic effects during flight due their high speeds. Functionally graded materials (FGMs), which enable continuous changes in material properties by varying the ratio of different materials, provide both thermal protection load-bearing capabilities. Therefore, they widely used structures for hypersonic vehicles. In this work, behaviors functionally (FG) plates under arbitrary temperature fields analyzed via a semianalytical method. This research develops method considering influence loading, specifically decrease stiffness stresses, as well correlation between temperatures fields, based on Ritz’s The classical plate theory, von–Karman’s large defection theory piston employed formulate strain energy, kinetic energy external work functions system. paper presents novel analysis static aerothermoelasticity FG plates, addition linear/nonlinear flutter such uniform, linear nonlinear fields. addition, volume fraction index, dynamic pressure, increase characteristics analyzed.

Язык: Английский

Процитировано

1

On the nonlinear mechanics of hybrid skew aerospace structures DOI
Hassan Mohammadi, Krzysztof Kamil Żur, Y. Kiani

и другие.

Aerospace Science and Technology, Год журнала: 2024, Номер unknown, С. 109624 - 109624

Опубликована: Сен. 1, 2024

Язык: Английский

Процитировано

1