Skip to main content

Advertisement

SpringerLink
Log in

Aerodynamics and blade flutter intelligent simulation of propeller vehicle under different wing angle

  • Original article
  • Published:
International Journal of System Assurance Engineering and Management Aims and scope Submit manuscript

Abstract

In recent years, with the development of aerospace field, composite materials show its importance and particularity in many fields and have a wide range of application potential because of its light weight structure. The application of composite materials to UAV blades can reduce the structural weight and improve the impact resistance. The mechanical properties, damage performance and failure mechanism of laminate under high strain rate are the fundaments for high-speed impact mechanics analysis. In this paper, a kind of fiber composite blade is designed independently, and the optimal laying angle is determined. Fluent is selected as the CFD calculation software to carry out the fluid–solid coupling analysis of the composite fixed wing. By changing the wing angle (0°, 10°, 17°, 24°), the flutter performance of the fixed wing under the condition of 45 m/s velocity flow is studied. The results show that the laminated laminate designed in this paper has longer action time under impact load, better protection for structure and better effect of resisting impact, and the trend and inflection point of stress and deformation of fixed wing are similar. Flutter occurs, the stress on the lower side of the fixed wing is larger than that on the upper side, and the stress on the outside is larger than that on the inside, and with the increase of time, the stress gradually spreads to both sides along the direction of the fixed wing. There is no correlation between the stress and strain of the fixed blade, and there is a threshold for the wing angle. When the wing angle is 10°, the blade has the smallest strain and the strongest wind resistance.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15
Fig. 16
Fig. 17
Fig. 18
Fig. 19
Fig. 20
Fig. 21
Fig. 22
Fig. 23

Similar content being viewed by others

References

  • Blocher M, May M, Schoenenborn H (2011) Dependency of unsteady time-linearized flutter investigations on the steady state flow field. ASME Turbo Expo, 2011, Vancouver, BC, Canada. GT2011-46500

  • Carrera E (2002) Theories and finite elements for multilayered, anisotropic, composite plates and shells. Arch Comput Methods Eng 9(2):87–140

    Article  MathSciNet  MATH  Google Scholar 

  • Carrera E (2003) Theories and finite elements for multilayered plates and shells: a unified compact formulation with numerical assessment and benchmarking. Arch Comput Methods Eng 10(3):215–296

    Article  MathSciNet  MATH  Google Scholar 

  • Carta FO (1967) Coupled blade-disk-shroud flutter instabilities in turbojet engine ro-tors. J Eng Power 89(3):419–426

    Article  Google Scholar 

  • Dong X et al (2020) Numerical simulations of flutter mechanism for high-speed wide-chord transonic fan. Aerosp Sci Technol 105:106009

    Article  Google Scholar 

  • Gadda A, Mangani L, Romanelli G, Mantegazza P, Casartelli E (2016) A GPU-accelerated compressible RANS solver for fluid-structure interaction simulations in turbomachinery. ISROMAC, 2016, Honolulu, HI, USA

  • Goerke D, Le Denmat A-L, Schmidt T, Kocian F, Nicke E (2012) Aerodynamic and mechanical optimization of CF/PEEK blades of a counter rotating fan. ASME Turbo Expo, 2012, Copenhagen, Denmark. GT2012-68797

  • Greenberg JM (1947) Airfoil in sinusoidal motion in pulsating stream. NACA TN 1326

  • Kim M, Vahdati M, Imregun M (2001) Aeroelastic stability analysis of a bird-damaged aeroengine fan assembly. Aerosp Sci Technol 5(7):469–482

    Article  MATH  Google Scholar 

  • Lee H-M, Hur N-K, Kwon O-J (2015) Aerodynamic design optimization of UAV rotor blades using a genetic algorithm

  • Liu YQ (2019) Analysis of practical application of carbon fiber composites in aerospace field. Bonding 40(07):69–71

    Google Scholar 

  • Mauffrey Y, Geeraert A, Verley S (2015) CROR blade deformation, part 2: aeroelastic computations and comparison with experiments. IFASD 2015, Saint Petersburg, Russia. IFASD-2015-043

  • Mauffrey Y, Geeraert A, Verley S (2015) CROR blade deformation, part 2: aeroelastic computations and comparison with experiments. IFASD, 2015, Saint Petersburg, Russia. IFASD-2015-043

  • Purushothaman K, Jeyaraman S K, Pratap A et al (2017) Aeroelastic flutter investigation and stability enhancement of a transonic axial compressor rotor using casing treatment. In: Asme Gas Turbine India Conference. 2017: V001T01A015.

  • Reed WH (1967) Review of propeller-rotor whirl flutter. NASA TR R-264

  • Schuff M, Lengyel-Kampmann T, Forsthofer N (2017) Influence of the steady deformation on numerical flutter prediction for highly loaded and flexible fan blades. In: ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers Digital Collection

  • Stepniewski WZ, Keys CN (1984) Rotary-wing aerodynamics. Courier Corporation

    Google Scholar 

  • Theodorsen T (1949) General theory of aerodynamic instability and the mechanics of flutter. NACA Report 496

  • Vahdati M et al (2001) Mechanisms and prediction methods for fan blade stall flutter. J Propul Power 17(5):1100–1108

    Article  Google Scholar 

  • Waite JJ, Kielb RE (2015) Physical understanding and sensitivities of low pressure turbine flutter. J Engi Gas Turbines Power 137(1):12502

    Article  Google Scholar 

  • Yoon S, Lee HC, Pulliam TH (2016) Computational study of flow interactions in coaxial rotors. AHS Technical Meeting on Aeromechanics Design for Vertical Lift

  • Yu HN, Gao CX, Wang YH (2020) Application and prospect of carbon fiber reinforced resin matrix composites. Synth Fiber Ind 543(1):55–59

    Google Scholar 

  • Zhang GY, Feng WM, Liu CL et al (2009) Numerical simulation of aerodynamic performance of six kinds of wind turbine blade airfoils. Renew Energy 27(2):11–15

    Google Scholar 

  • Zhu CF, Lin Z, Xie JY et al (2020) Analysis of aerodynamic characteristics of coaxial twin rotors of UAV. Shanxi Electron Technol 95:105645

    Google Scholar 

Download references

Acknowledgements

I would first like to thank Professor Zongjie Cao for his guiding comments and suggestions on the research direction of my dissertation, and for his timely and attentive guidance on the difficulties and doubts I encountered during the writing of my dissertation, and for his many helpful suggestions for improvement. In addition, I am greatly inspired by the strong support and help provided by Yang Shuai in the preparation of the thesis. I would also like to thank the authors in the references, through their research articles, which gave me a good starting point for my research topic.

Funding

There is no funding for this paper.

Author information

Authors and Affiliations

  1. Aviation University Air Force, Changchun, China

    Leilei Yu & Zongjie Cao

  2. Unit 78102, Chengdu, China

    Shuai Yang

Authors
  1. Leilei Yu
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Zongjie Cao
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Shuai Yang
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Leilei Yu.

Ethics declarations

Conflict of interest

The authors declare no conflict of interest.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Yu, L., Cao, Z. & Yang, S. Aerodynamics and blade flutter intelligent simulation of propeller vehicle under different wing angle. Int J Syst Assur Eng Manag 14, 657–669 (2023). https://doi.org/10.1007/s13198-021-01457-5

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s13198-021-01457-5

Keywords

Search

Navigation