OpenAlex Citation Counts

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OpenAlex is a bibliographic catalogue of scientific papers, authors and institutions accessible in open access mode, named after the Library of Alexandria. It's citation coverage is excellent and I hope you will find utility in this listing of citing articles!

If you click the article title, you'll navigate to the article, as listed in CrossRef. If you click the Open Access links, you'll navigate to the "best Open Access location". Clicking the citation count will open this listing for that article. Lastly at the bottom of the page, you'll find basic pagination options.

Requested Article:

Mechanism of single-mode panel flutter in low supersonic flow
Liuqing Ye, Kun Ye, Ke Jin, et al.
Aerospace Science and Technology (2024) Vol. 147, pp. 109002-109002
Closed Access | Times Cited: 6

Showing 6 citing articles:

A novel FSI model of composite blisk with blades-disk coupling and ROM-based for flutter analysis
Qian Xu, Lei Hou, Lixian Hou, et al.
Aerospace Science and Technology (2025), pp. 109961-109961
Closed Access

Single-mode flutter analysis of drag reduction spike by parameterized eigenvalue method and energy method
Chengde Huang, Xiangyan Chen, Xueyuan Nie, et al.
Aerospace Science and Technology (2024) Vol. 155, pp. 109736-109736
Closed Access | Times Cited: 1

A novel tensor-based modal decomposition method for reduced order modeling and optimal sparse sensor placement
Zhirong Zhong, Xuanhao Hua, Zhi Zhai, et al.
Aerospace Science and Technology (2024) Vol. 155, pp. 109530-109530
Closed Access

Flutter Mechanism of a Thin Plate Considering Attack Angles
Chengjun Yan, Qi Wang, Bo Wu, et al.
Applied Sciences (2024) Vol. 14, Iss. 20, pp. 9380-9380
Open Access

Optimization flutter response of laminated smart nanocomposite truncated conical shell under supersonic aerodynamic pressure using hybrid IGWO-DQHFEM
L. Shan, M. Furjan, Reza Kolahchi, et al.
Aerospace Science and Technology (2024), pp. 109766-109766
Closed Access

Active aero-visco-elastic flutter control and layerwise modelling of supersonic smart sandwich panels with variable stiffness composites
J.A. Moreira, F. Moleiro, A.L. Araújo, et al.
Aerospace Science and Technology (2024) Vol. 157, pp. 109847-109847
Open Access

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