Skip to main content
Log in

Lattice Boltzmann Method used for the aircraft characteristics computation at high angle of attack

  • Published:
Science China Technological Sciences Aims and scope Submit manuscript

Abstract

Traditional Finite Volume Method (FVM) and Lattice Boltzmann Method (LBM) are both used to compute the high angle attack aerodynamic characteristics of the benchmark aircraft model named CT-1. Even though the software requires flow on the order of Ma < 0.4, simulation at Ma=0.5 is run in PowerFLOW after theoretical analysis. The consistency with the wind tunnel testing is satisfied, especially for the LBM which can produce perfect results at high angle attack. PowerFLOW can accurately capture the detail of flows because it is inherently time-dependent and parallel and suits large-scale computation very well.

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

Access this article

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

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Qian Y J. AeroDynamics (in Chinese), Beijing: BUAA Press, 2004

    Google Scholar 

  2. Wu J Q, Fan Z L, He Z, et al. Research on the tests technology at high angles of attack in 2. 4m transonic wind tunnel (in Chinese). Exp Meas Fluid Mech, 2004, 18: 43–48

    Google Scholar 

  3. Wang F J. Analysis of Computational Fluid Dynamics (in Chinese). Beijing: Tsinghua University Press, 2006

    Google Scholar 

  4. Wu W Y. Fluid Mechanics (in Chinese), Beijing: Peking University Press, 1983

    Google Scholar 

  5. Anderson J D Jr. Computational Fluid Dynamics—The Basics with Applications. Beijing: Tsinghua University Press, 2002

    Google Scholar 

  6. Li X Q. The computation of a wing-body combination with aileron (in Chinese). Acta Aerodyn Sin, 2004, 22: 337–341

    Google Scholar 

  7. Li X Q. Numerical aerodynamic analysis of a high speed airplane (in Chinese). J Hydrodyn, 2004, 19: 838–848

    Google Scholar 

  8. Qian Y H, d’Humieres D, Lallemand P. Lattice BGK Models for Navier Stokes Equations. Euro Phys Lett, 1992, 17: 479–484

    Article  MATH  Google Scholar 

  9. Chen H D. Kinetic Theory Based Approach for CFD, MA USA: EXA Corporation, 2004

    Google Scholar 

  10. Shan X W, Yuan X F, Chen H D. Kinetic theory representation of hydrodynamics: a way beyond the N-S equation. J Fluid Mech, 2006, 550: 413–441

    Article  MATH  MathSciNet  Google Scholar 

  11. Cummings R M, Forsythe J R, Morton S A, et al. Computational challenges in high angle of attack flow prediction. Progr Aerospace Sci, 2003, 39: 369–384

    Article  Google Scholar 

  12. Chen H D, Kandasamy S, Orszag S, et al. Extended Boltzmann kinetic equation for turbulent flows. Science, 2003, 301: 633–636

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to YiWei Wang.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Du, T., Li, X., Zhang, X. et al. Lattice Boltzmann Method used for the aircraft characteristics computation at high angle of attack. Sci. China Technol. Sci. 53, 2068–2073 (2010). https://doi.org/10.1007/s11431-010-3222-2

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11431-010-3222-2

Keywords

Navigation