Technical Papers
Jan 31, 2024

Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip

Publication: Journal of Aerospace Engineering
Volume 37, Issue 3

Abstract

The use of flared folding wingtip (FFWT) for load alleviation has been considered in recent studies. Most studies analyzed FFWT based on the linear assumption and ignored the nonlinearity of large wingtip folding angle. In this paper, for FFWT, a nonlinear aeroelastic modeling method based on multibody dynamics and unsteady vortex lattice method (UVLM) is developed. For wing with free-float FFWT, equilibrium and gust responses are simulated, and the gust responses were compared to the results of wind tunnel test to verify the validity of this method. The simulation results show that the geometric nonlinearity of the wingtip has little effect on the main wing but obvious effect on the wingtip. For a wing with active wingtip, the responses excited by wingtip active folding are simulated and compared to the linear modal method, which shows that the nonlinearity has large effects on the wing, especially at low excitation frequencies, and may lead to occurrence of response frequencies different from excitation.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

References

Attar, P. J., D. Tang, and E. H. Dowell. 2010. “Nonlinear aeroelastic study for folding wing structures.” AIAA J. 48 (10): 2187–2195. https://doi.org/10.2514/1.44868.
Balatti, D., J. D. Ellis, S. JiffrI, H. Haddad Khodaparast, and M. I. Friswell. 2023a. “Active hinged wingtip for gust load alleviation and manoeuvres.” In Proc., AIAA SciTech Forum 2023, 2023–2567. Reston, VA: American Institute of Aeronautics and Astronautics.
Balatti, D., H. H. Khodaparast, M. I. Friswell, M. Manolesos, and A. Castrichini. 2023b. “Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation.” J. Fluids Struct. 119 (May): 103892. https://doi.org/10.1016/j.jfluidstructs.2023.103892.
Barbarino, S., O. Bilgen, R. M. Ajaj, M. I. Friswell, and D. J. Inman. 2011. “A review of morphing aircraft.” J. Intell. Mater. Syst. Struct. 22 (9): 823–877. https://doi.org/10.1177/1045389X11414084.
Bourdin, P., A. Gatto, and M. Friswell. 2006. “The application of variable cant angle winglets for morphing aircraft control.” In Proc., 24th AIAA Applied Aerodynamics Conf., Reston, VA: American Institute of Aeronautics and Astronautics.
Bourdin, P., A. Gatto, and M. I. Friswell. 2008. “Aircraft control via variable cant-angle winglets.” J. Aircr. 45 (2): 414–423. https://doi.org/10.2514/1.27720.
Bourdin, P., A. Gatto, and M. I. Friswell. 2010. “Performing co-ordinated turns with articulated wing-tips as multi-axis control effectors.” Aeronaut. J. 114 (1151): 35–47. https://doi.org/10.1017/S0001924000003511.
Castrichini, A., J. E. Cooper, T. Wilson, A. Carrella, and Y. Lemmens. 2017a. “Nonlinear negative stiffness wingtip spring device for gust loads alleviation.” J. Aircr. 54 (2): 627–641. https://doi.org/10.2514/1.C033887.
Castrichini, A., V. Hodigere Siddaramaiah, D. E. Calderon, J. E. Cooper, T. Wilson, and Y. Lemmens. 2016. “Nonlinear folding wing tips for gust loads alleviation.” J. Aircr. 53 (5): 1391–1399. https://doi.org/10.2514/1.C033474.
Castrichini, A., V. H. Siddaramaiah, D. E. Calderon, J. E. Cooper, T. Wilson, and Y. Lemmens. 2017b. “Preliminary investigation of use of flexible folding wing tips for static and dynamic load alleviation.” Aeronaut. J. 121 (1235): 73–94. https://doi.org/10.1017/aer.2016.108.
Cheung, R. C., D. Rezgui, J. E. Cooper, and T. Wilson. 2018. “Testing of a hinged wingtip device for gust loads alleviation.” J. Aircr. 55 (5): 2050–2067. https://doi.org/10.2514/1.C034811.
Cheung, R. C., D. Rezgui, J. E. Cooper, and T. Wilson. 2020. “Testing of folding wingtip for gust load alleviation of flexible high-aspect-ratio wing.” J. Aircr. 57 (5): 876–888. https://doi.org/10.2514/1.C035732.
Conti, C., F. Saltari, F. Mastroddi, T. Wilson, and A. Castrichini. 2021. “Quasi-steady aeroelastic analysis of the semi-aeroelastic hinge including geometric nonlinearities.” J. Aircr. 58 (5): 1168–1178. https://doi.org/10.2514/1.C036115.
Harder, R. L., and R. N. Desmarais. 1972. “Interpolation using surface splines.” J. Aircr. 9 (2): 189–191. https://doi.org/10.2514/3.44330.
Healy, F., R. Cheung, D. Rezgui, and J. Cooper. 2022a. “Nonlinear stability analysis and experimental exploration of limit cycle oscillations with flared folding wingtips.” In Proc., AIAA SciTech Forum 2022, 1–18. Reston, VA: American Institute of Aeronautics and Astronautics.
Healy, F., R. Cheung, D. Rezgui, J. Cooper, T. Wilson, and A. Castrichini. 2022b. “On the effect of geometric nonlinearity on the dynamics of flared folding wingtips.” J. Aircr. 60 (2): 368–381. https://doi.org/10.2514/1.C036877.
Katz, J., and A. Plotkin. 2001. Low-speed aerodynamics: From wing theory to panel method. 2nd ed. Cambridge, UK: Cambridge University Press.
Lee, D. H., and T. A. Weisshaar. 2005. “Aeroelastic studies on a folding wing configuration.” In Proc., 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conf. Reston, VA: American Institute of Aeronautics and Astronautics.
Love, M. H., P. S. Zink, R. L. Stroud, D. R. Bye, and C. Chase. 2004. “Impact of actuation concepts on morphing aircraft structures.” In Proc., 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conf. Reston, VA: American Institute of Aeronautics and Astronautics.
Mastracci, P., F. Saltari, F. Mastroddi, T. Wilson, and A. Castrichini. 2022. “Unsteady aeroelastic analysis of the semi aeroelastic hinge including local geometric nonlinearities.” AIAA J. 60 (5): 3147–3165. https://doi.org/10.2514/1.J061108.
Shabana, A. A. 2013. Dynamics of multibody systems. 4th ed. Cambridge, UK: Cambridge University Press.
Tang, D., and E. H. Dowell. 2008. “Theoretical and experimental aeroelastic study for folding wing structures.” J. Aircr. 45 (4): 1136–1147. https://doi.org/10.2514/1.32754.
Wilson, T., J. Kirk, J. Hobday, and A. Castrichini. 2019. “Small scale flying demonstration of semi aeroelastic hinged wing tips.” In Proc., Int. Forum on Aeroelasticity and Structural Dynamics 2019. Red Hook, NY: Curran Associates.
Yue, C., and Y. Zhao. 2021. “Interpolation-based modeling methodology for efficient aeroelastic control of a folding wing.” Int. J. Aerosp. Eng. 2021 (2021): 1–20. https://doi.org/10.1155/2021/8609211.
Zhao, Y., and H. Hu. 2012. “Parameterized aeroelastic modeling and flutter analysis for a folding wing.” J. Sound Vib. 331 (2): 308–324. https://doi.org/10.1016/j.jsv.2011.08.028.
Zhao, Y., and H. Hu. 2013. “Prediction of transient responses of a folding wing during the morphing process.” Aerosp. Sci. Technol. 24 (1): 89–94. https://doi.org/10.1016/j.ast.2011.09.001.

Information & Authors

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 3May 2024

History

Received: Jun 8, 2023
Accepted: Oct 24, 2023
Published online: Jan 31, 2024
Published in print: May 1, 2024
Discussion open until: Jun 30, 2024

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Junhui Han
Ph.D. Student, School of Aeronautic Science and Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.
Professor, School of Aeronautic Science and Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China (corresponding author). Email: [email protected]
Chao Yang
Professor, School of Aeronautic Science and Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

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