Skip to main content
Log in

Steady vortex force theory and slender-wing flow diagnosis

  • Research Paper
  • Published:
Acta Mechanica Sinica Aims and scope Submit manuscript

Abstract

The concept vortex force in aerodynamics is systematically examined based on a new steady vortex-force theory (Wu et al., Vorticity and vortex dynamics, Springer, 2006) which expresses the aerodynamic force (and moment) by the volume and boundary integrals of the Lamb vector. In this paper, the underlying physics of this theory is explored, including the general role of the Lamb vector in nonlinear aerodynamics, its initial formation, and its relevance to the total-pressure non-uniformity. As a typical example, the theory is applied to the flow over a slender delta wing at a large angle of attack. The highly localized flow structures with high Lamb-vector peaks are identified in terms of their net contribution to various constituents of the total aerodynamic force. This vortex-force diagnosis sheds new light on the flow control and configuration optimization.

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. Prandtl, L., Tragflügeltheorie, I.: Mitteilungen, Nachrichten Ges. Wiss. Göttingen, Math-Phys. Kl. 151–177 (Also: Gesammelte Abhandlungen, vol. 1, pp. 322–345) (1918)

  2. Kármán, T., von Burgers, J.M.: General aerodynamic theory, perfect fluids. Aerodynamic Theory. Durand ed. vol. II, Stanford (1934)

  3. Lighthill M.J. (1962). Physical intergretation of the mathematical theory of wave generation by wing. J. Fluid Mech. 14: 385–398

    Article  MATH  MathSciNet  Google Scholar 

  4. Saffman P.G. (1992). Vortex Dynamics. Cambridge University Press, Cambridge

    MATH  Google Scholar 

  5. Wu J.Z., Ma H.Y. and Zhou M.D. (2006). Vorticity and Vortex Dynamics. Springer, Heidelberg

    Google Scholar 

  6. Wu J.C. (2005). Elements of Vorticity Aerodynamics. Tsinghua University Press, Beijing

    Google Scholar 

  7. Wu J.Z., Zhou Y., Lu X.Y. and Fan M. (1999). Turbulent force as a diffusive field with vortical sources. Phys. Fluids 11: 627–635

    Article  MathSciNet  Google Scholar 

  8. Lighthill M.J. (1986). An Informal Introduction to Theoretical Fluid Mechanics. Clarendon Press, Oxford

    MATH  Google Scholar 

  9. Wu, J.M., Ondrusek, B., Wu, J.Z.: Exact force diagnostics of vehicles based on wake-plane data. AIAA 96-0559 (1996)

  10. Lee M. and Ho C.M. (1990). Lift force of delta wings. Appl. Mech. Rev. 43(9): 209–221

    Google Scholar 

  11. Wu J.Z., Lu X.Y. and Zhuang L.X. (2006). Integral force acting on a body due to local flow structures. J. Fluid Mech. 576: 265–286

    Article  MathSciNet  Google Scholar 

  12. Wu, J.Z., Wu, J.M.: Vortical sourses of aerodynamics force and moment. SAE 89-2346 (1989)

  13. Wu, J.Z., Roach, R.L., Lo, C.F., Zhu, F.L.: Aerodynamic diagnosis and design based on boundary vorticity dynamics. AIAA 99-3103 (1999)

  14. Luo, Y.B.: Boundary vorticity dynamics, derivative-moment theory and their application in flow diagnosis and control (in Chinese). Master dissertation, Peking University, Beijing (2004)

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to J. Z. Wu.

Additional information

The project supported partly by the National Natural Science Foundation of China (10572005).

Rights and permissions

Reprints and permissions

About this article

Cite this article

Yang, Y.T., Zhang, R.K., An, Y.R. et al. Steady vortex force theory and slender-wing flow diagnosis. Acta Mech. Sin. 23, 609–619 (2007). https://doi.org/10.1007/s10409-007-0107-0

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10409-007-0107-0

Keywords

Navigation