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Effects of 3-D deformation of elastic wings on aerodynamic performance of an aircraft model

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Abstract

The wind tunnel experiment is conducted on a simplified aircraft model with rigid and two kinds of elastic wings to investigate the effect of wing 3-D deformation on the aircraft aerodynamic performance. The results show that two elastic wings exhibit different aerodynamic performances, which are classified as the lift-enhancement wing and the drag-reduction wing. For the lift-enhancement wing, the stall angle is delayed from 8° to 15° with a corresponding lift increment of 64.3% compared with the rigid wing. It is shown that the lift enhancement of the aircraft model is accompanied by the torsional vibration mode of the wing, which results in the significant improvement of wing circulation. For the drag-reduction wing, the aerodynamic performance is dominated by the time-averaged deformation, which couples the bending and twisting. The wing twist reduces the effective angle of attack, as well as the frontal area, and contributes to the decreased wake deficit. Meantime, the bent wings function as barriers to the cross flow resulting in a reduction of lift-induced drag. As a result, the drag coefficient is reduced from 0.115 to 0.098 with a reduction of 14.8% at angle of attack of 12°.

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References

  1. Shyy W, Ifju P, Viieru D. Membrane wing-based micro air vehicles. Appl Mech Rev, 2005, 58: 283–301

    Article  Google Scholar 

  2. Taylor G, Wang Z, Vardaki E, et al. Lift enhancement over flexible nonslender delta wings. AIAA J, 2007, 45: 2979–2993

    Article  Google Scholar 

  3. Fu J, Liu X, Shyy W, et al. Effects of flexibility and aspect ratio on the aerodynamic performance of flapping wings. Bioinspir Biomim, 2018, 13: 036001

    Article  Google Scholar 

  4. Tiomkin S, Raveh D E. A review of membrane-wing aeroelasticity. Prog Aerospace Sci, 2021, 126: 100738

    Article  Google Scholar 

  5. Anderson J D. Aircraft Performances and Design. 2nd ed. New York: McGraw Hill, 1996. 18–19

    Google Scholar 

  6. Song A, Tian X, Israeli E, et al. Aeromechanics of membrane wings with implications for animal flight. AIAA J, 2008, 46: 2096–2106

    Article  Google Scholar 

  7. Rojratsirikul P, Wang Z, Gursul I. Unsteady fluid-structure interactions of membrane airfoils at low Reynolds numbers. Exp Fluids, 2009, 46: 859–872

    Article  Google Scholar 

  8. Bleischwitz R, de Kat R, Ganapathisubramani B. On the fluid-structure interaction of flexible membrane wings for MAVs in and out of ground-effect. J Fluids Struct, 2017, 70: 214–234

    Article  Google Scholar 

  9. He X, Wang J J. Fluid—structure interaction of a flexible membrane wing at a fixed angle of attack. Phys Fluids, 2020, 32: 127102

    Article  Google Scholar 

  10. Béguin B, Breitsamter C, Adams N A. Aerodynamic investigations of a morphing membrane wing. AIAA J, 2012, 50: 2588–2599

    Article  Google Scholar 

  11. Guo Q, He X, Wang Z, et al. Effects of wing flexibility on aerodynamic performance of an aircraft model. Chin J Aeronautics, 2021, 34: 133–142

    Article  Google Scholar 

  12. Pflüger J, Breitsamter C. Experimental investigations of a full model with adaptive elasto-flexible membrane wing. Chin J Aeronaut, 2021, 34: 211–218

    Article  Google Scholar 

  13. Masoud H, Alexeev A. Resonance of flexible flapping wings at low Reynolds number. Phys Rev E, 2010, 81: 1–5

    Article  Google Scholar 

  14. Dai H, Luo H, Doyle J F. Dynamic pitching of an elastic rectangular wing in hovering motion. J Fluid Mech, 2012, 693: 473–499

    Article  MATH  Google Scholar 

  15. Ramananarivo S, Godoy-Diana R, Thiria B. Rather than resonance, flapping wing flyers may play on aerodynamics to improve performance. Proc Natl Acad Sci USA, 2011, 108: 5964–5969

    Article  Google Scholar 

  16. Cleaver D J, Calderon D, Wang Z, et al. Low aspect ratio oscillating flexible wings at low Reynolds numbers. In: 43rd Fluid Dynamics Conference. San Diego, California, 2013. AIAA-2013-3178

  17. Gursul I, Cleaver D J, Wang Z. Control of low Reynolds number flows by means of fluid-structure interactions. Prog Aerospace Sci, 2014, 64: 17–55

    Article  Google Scholar 

  18. Taylor G, Kroker A, Gursul I. Passive flow control over flexible nonslender delta wings. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada, 2005. AIAA-2005-0865

  19. Wang J J, Wu K. Experimental investigations of the effect of wing elastic deformations on aerodynamics. Acta Aerodynamica Sinica, 2007, 25: 55–59

    Google Scholar 

  20. Feng S Y, Guo Q F, Wang J J, et al. Influence of membrane wing active deformation on the aerodynamic performance of an aircraft model. Sci China Tech Sci, 2022, 65: 2474–2484

    Article  Google Scholar 

  21. Zhan J X, Wang J J. The effect of leading-edge sweep angle asymmetry on lateral aerodynamics. Sci China Ser E-Technol Sci, 2009, 52: 2445–2448

    Article  Google Scholar 

  22. Zhan J X. Experimental investigation on the aerodynamic performance and mechanism of MAV configurations based on common swift. Dissertation for the Doctoral Degree. Beijing: Beihang University, 2007

    Google Scholar 

  23. Gorlin S M, Slezinger I I. Aerodynamic Measurements: Methods and Instrumentation. Moscow: Nauka, 1964. 36

    Google Scholar 

  24. Chen T Y, Liou L R. Blockage corrections in wind tunnel tests of small horizontal-axis wind turbines. Exp Thermal Fluid Sci, 2011, 35: 565–569

    Article  Google Scholar 

  25. Takeda M, Mutoh K. Fourier transform profilometry for the automatic measurement of 3-D object shapes. Appl Opt, 1983, 22: 3977–3982

    Article  Google Scholar 

  26. Champagnat F, Plyer A, Le Besnerais G, et al. Fast and accurate PIV computation using highly parallel iterative correlation maximization. Exp Fluids, 2011, 50: 1169–1182

    Article  Google Scholar 

  27. Pan C, Xue D, Xu Y, et al. Evaluating the accuracy performance of Lucas-Kanade algorithm in the circumstance of PIV application. Sci China-Phys Mech Astron, 2015, 58: 1–16

    Article  Google Scholar 

  28. Lee T, Su Y Y. Wingtip vortex control via the use of a reverse half-delta wing. Exp Fluids, 2012, 52: 1593–1609

    Article  Google Scholar 

  29. Shi X D, Feng L H. Control of flow around a circular cylinder by bleed near the separation points. Exp Fluids, 2015, 56: 1–17

    Article  Google Scholar 

  30. Maskell E C. Progress towards a method for the measurement of the components of the drag of a wing of finite span. RAE Technical Report 72232. 1972

  31. Kusunose K, Crowder J P. Physical properties of Maskell’s induced drag integral. In: 39th AIAA Aerospace Sciences Meeting & Exhibit. Reno, Nevada, 2001. AIAA-2001-0421

  32. Brune G W. Quantitative low-speed wake surveys. J Aircraft, 1994, 31: 249–255

    Article  Google Scholar 

  33. Kusunose K. Development of a universal wake survey data analysis code. In: 15th Applied Aerodynamics Conference. Atlanta, Georgia, 1997. AIAA-97-2294

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Authors and Affiliations

  1. Fluid Mechanics Key Laboratory of Education Ministry, Beijing University of Aeronautics and Astronautics, Beijing, 100191, China

    QinFeng Guo, SiYuan Feng & JinJun Wang

Authors
  1. QinFeng Guo
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  2. SiYuan Feng
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  3. JinJun Wang
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Correspondence to JinJun Wang.

Additional information

This work was supported by the National Natural Science Foundation of China (Grant Nos. 12127802 and 11721202) and the Academic Excellence Foundation of Beijing University of Aeronautics and Astronautics (BUAA) for PhD Students.

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Guo, Q., Feng, S. & Wang, J. Effects of 3-D deformation of elastic wings on aerodynamic performance of an aircraft model. Sci. China Technol. Sci. 66, 1365–1377 (2023). https://doi.org/10.1007/s11431-022-2323-x

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  • DOI: https://doi.org/10.1007/s11431-022-2323-x

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