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All issues Volume 42 / No 2 (April 2024) JNWPU, 42 2 (2024) 241-250 References
Open Access
Issue
JNWPU
Volume 42, Number 2, April 2024
Page(s) 241 - 250
DOI https://doi.org/10.1051/jnwpu/20244220241
Published online 30 May 2024
  1. XIANG Jinwu, KAN Zi, SHAO Haoyuan, et al. A review of key technologies for long-endurance unmanned aerial vehicle[J]. Journal of Harbin Institute of Technology, 2020, 52(6): 57–77 [Article] (in Chinese) [Google Scholar]
  2. CHEN Yingchun, ZHANG Meihong, ZHANG Miao, et al. Review of large civil aircraft aerodynamic design[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(1): 35–51 [Article] (in Chinese) [Google Scholar]
  3. YANG Chao, QIU Qisheng, ZHOU Yitao, et al. Review of aircraft gust response mitigation techniques[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 216–256 (in Chinese) [Google Scholar]
  4. AJAJ R M, PARANCHEERIVILAKKATHIL M S, AMOOZGAR M R, et al. Recent developments in the aeroelasticity of morphing aircraft[J]. Progress in Aerospace Sciences, 2020, 120(10): 682–702 [Google Scholar]
  5. SIDDARAMAIAH V H. Preliminary studies in the use of folding wing-tips for loads alleviation[C]//Applied Aerodynamics Conference, 2014 [Google Scholar]
  6. CASTRICHINI A, HODIGERE S V, CALDERON D E, et al. Preliminary investigation of use of flexible folding wing-tips for static and dynamic loads alleviation[C]//4th RAES Aircraft Structural Design Conference, 2014 [Google Scholar]
  7. CASTRICHINI A, COOPER J E, WILSON T, et al. Nonlinear negative stiffness wingtip spring device for gust loads alleviation[J]. Journal of Aircraft, 2017, 54(2): 368–383 [Google Scholar]
  8. AJAJ R M. Flight dynamics of transport aircraft equipped with flared-hinge folding wingtips[J]. Journal of Aircraft, 2020, 58(1): 213–224 [Google Scholar]
  9. VALENTE C, CASTRICHINI A, WILSON T, et al. High fidelity CFD/CSM analysis of a folding wing-tip device for aircraft loads alleviation[C]//6th Aircraft Structural Design Conference, 2018 [Google Scholar]
  10. CHEUNG R C M, REZGUI D, COOPER J E, et al. Testing of a hinged wingtip device for gust loads alleviation[J]. Journal of Aircraft, 2018, 55(5): 2050–2067 [CrossRef] [Google Scholar]
  11. THOMAS W, JAMES K, JOHN H, et al. Small scale flying demonstration of semi aeroelastic hinged wing tip[C]//18th International Forum on Aeroelasticity and Structural Dynamics, Savannah, 2019 [Google Scholar]
  12. YANG Ning, WU Zhigang, YANG Chao, et al. Flutter analysis of a folding wing with structural nonlinearity[J]. Engineering Mechanics, 2012, 29(2): 197–204 [Article] (in Chinese) [Google Scholar]
  13. XU Hao, HAN Jinlong, XI Yong, et al. Aeroelastic morphing flight simulation platform for folding wing[J/OL]. (2022-11-23)[2023-01-05]. http://kns.cnki.net/kcms/detail/11.2625.V.20221103.1727.004.html (in Chinese) [Google Scholar]
  14. ZHAN Jiuyu, ZHOU Xinghua, HUANG Rui. Parametric aeroelastic modeling of folding wing based on manifold tangent space interpolation[J]. Chinese Journal of Theoretical and Applied Mechanics, 2021, 53(4): 1103–1113 [Article] (in Chinese) [Google Scholar]
  15. LIU Xiangyi, YAN Yongju, WEN Baiheng, et al. Research on gust response and passive alleviation of flexible wing[J]. Journal of Naval Aviation University, 2016, 31(6): 635–640 (in Chinese) [Google Scholar]
  16. XIAO Ling. The method of partial dynamic equivalence and aeroelasticity research in folding wing tip[D]. Dalian: Dalian University of Technology, 2021: 59–66 (in Chinese) [Google Scholar]
  17. WAN Zhiqiang, TANG Changhong, ZOU Congqing. Static aeroelastic characteristics analysis of a flexible forward swept composite aircraft[J]. Acta Materiae Compositae Sinica, 2002(5): 118–124 [Article] (in chinese) [Google Scholar]
  18. RODDEN W P, JOHNSON E H. MSC/Nastran aeroelastic analtsis user's guide V68[M]. Log Angeles: MSC Coporation, 1994 [Google Scholar]
  19. FULLER J R. Evolution and future development of airplane gust loads design requirements[C]//World Aviation Congress, 1997 [Google Scholar]
  20. MASTRACCI P, SALTARI F, MASTRODDI F, et al. Unsteady aeroelastic analysis of the semi aeroelastic hinge including local geometric nonlinearities[J]. AIAA Journal, 2022, 60(5): 3147n3165 [NASA ADS] [CrossRef] [Google Scholar]

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