Dan Wang


  1. [1] G. Yang, H. Guo, H. Xiao, H. Jiang, and R. Liu, Out-of-planestiffness analysis of kevlar/carbon fiber hybrid composite skinsfor a shear variable-swept wing, Applied Composite Materials,28, 2021, 1653–1673.
  2. [2] M. Uzun, H.H. Bilgic, E.H. C¸opur, and S. Coban, Theaerodynamic force estimation of a swept-wing UAV usingANFIS based on metaheuristic algorithms, The AeronauticalJournal, 23(8), 2023, 1–17.
  3. [3] J. George and G. Mani, HiL implementation of harmony search-based redesigned pi-like control for dc servo, MechatronicSystems and Control, 51(1), 2023, 25–33.
  4. [4] C.H.U. Lingling, L.I. Qi, G.U. Feng, D.U. Xintian, H.E. Yuqing,and D.E.N.G. Yangchen, Design, modeling, and control ofmorphing aircraft: A review, Chinese Journal of Aeronautics,35(5), 2022, 220–246.
  5. [5] Y. Gao, Y. Li, Y. Wang, Z. Zhang, and R. Lu, Researchon variable swept wing mode of missile based on fluttercharacteristics, Journal of System Simulation, 33(5), 2021,12–24.
  6. [6] Z. Zhou and J. Huang, Auto sweptback wing based on lowscattering demand for an unmanned aerial vehicle in phaseflight, Aerospace, 9(12), 2022, 757.
  7. [7] L. Zhang and Y. Zhao, Time-varying aeroelastic modeling andanalysis of a rapidly morphing wing, Aerospace, 10(2), 2023,20–197.
  8. [8] Y. Lu, J. Hu, G. Chen, A. Liu, and J. Feng, Optimization ofwater-entry and water-exit maneuver trajectory for morphingunmanned aerial-underwater vehicle, Ocean Engineering,261(10), 2022, 15–112.
  9. [9] A.A. Shanyavskiy, A.P. Soldatenkov, and A.A. Toushentsov,Foundation of damage tolerance principles in-Service for theRRJ aircraft structural components, Fatigue & Fracture ofEngineering Materials & Structures, 44(10), 2021, 2827–2844.
  10. [10] O.Y. Al-Thehabey, Dynamic instability analysis of aeroelasticsystems with application to aircraft wings, Physics of Fluids,33(9), 2021, 2–19.
  11. [11] H. Li, G. Li, Q. Wang, B. Ju, and Y. Wen, Friction torquefield distribution of a permanent-magnet spherical motor basedon multi-physical field coupling analysis, IET Electric PowerApplications, 15(8), 2021, 1045–1055.
  12. [12] C. Yan, Y. Li, Y. Cheng, J. Wei, W. Tian, S. Li, and Z.Wang, Multifield coupling mechanism in formations around awellbore during the exploitation of methane hydrate with CO2replacement, Energy, 245(15), 2022, 2–13.
  13. [13] D. Laya, S. Dutta, and S. Chakraborty, Quantum cosmologyin coupled Brans–Dicke gravity: A Noether symmetry analysis,International Journal of Modern Physics D, 32(02), 2023,2–16.
  14. [14] W. Feng, R. Jiang, H. Chen, S. Qiang, Z. Gong, Z. Li, J.Pan, W. Zhao, X. Zhang, X. Luo, and X. Zhang, Developmentof a multi-physics coupling system based on ICoCo interfaceand its validation on NEA-OECD core transient benchmark,Annals of Nuclear Energy, 156(6), 2021, 2–7.
  15. [15] Y. Yuan, M. Zheng, H. Xue, Z. Duan, and W. Tang, Fatigueanalysis of a steel catenary riser at touchdown zone withseabed resistance and hydrodynamic forces, Ocean Engineering,244(15), 2022, 2–10.
  16. [16] Z. Yang, L. Sun, C. Zhang, and C. Gao, Analysis of acomposite piezoelectric semiconductor cylindrical shell underthe thermal loading, Mechanics of Materials, 164(1), 2022,2–10.
  17. [17] S. Tang, X. Liu, C. Wang, D. Zhang, G H. Su, W. Tian, and S.Qiu, Thermal-electrical coupling characteristic analysis of theheat pipe cooled reactor with static thermoelectric conversion,Annals of Nuclear Energy, 168(4), 2022, 2–13.
  18. [18] L. Liu, X. Guo, and C. Lee, Promoting smart cities into the5G era with multi-field Internet of Things (IoT) applicationspowered with advanced mechanical energy harvesters, NanoEnergy, 88(10), 2021, 106–304.
  19. [19] D. Aikhuele, Development of a statistical reliability-basedmodel for the estimation and optimization of a spur gearsystem, Journal of Computational and Cognitive Engineering,2(2), 2022, 168–174.
  20. [20] G. Yao, M. Song, and L. Zhu, Time-varying stability andvibration of an embedded thin plate on a swept wing, AerospaceScience and Technology, 140(9), 2023, 108–436.
  21. [21] X. Wang, J. Gong, and Y. Wang, Research on optimal guidancelaw with landing angle constraint, Mechatronic Systems andControl, 51(2), 2023, 79–85.
  22. [22] R. Xia, S. Gao, and D. Zhao, A terminal sliding mode learningcontrol for a class of uncertain non-linear systems, MechatronicSystems and Control, 50(2), 2022, 87–95.
  23. [23] Y. Kishi, M. Kanazaki, and Y. Makino, Supersonic forward-swept wing design using multifidelity efficient global optimiza-tion, Journal of Aircraft, 59(4), 2022, 1027–1040.

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