Skip to main content
Log in

Transitional intermittency in boundary layers subjected to pressure gradient

  • Published:
Experiments in Fluids Aims and scope Submit manuscript

Summary

Results are reported from an extensive series of experiments on boundary layers in which the location of pressure gradient and transition onset could be varied almost independently, by judicious use of tunnel wall liners and transition-fixing devices. The experiments show that the transition zone is sensitive to the pressure gradient especially near onset, and can be significantly asymmetric; no universal similarity appears valid in general. Observed intermittency distributions cannot be explained on the basis of the hypothesis, often made, that the spot propagates at speeds proportional to the local free-stream velocity but is otherwise unaffected by the pressure gradient.

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

  • Abu-Ghannam, J. B.; Shaw, R. I. 1980: Natural transition of boundary layers — the effects of turbulence, pressure gradient and flow history. J. Mech. Eng. Sci. 22, 213–238

    Google Scholar 

  • Chen, K. K.; Thyson, N. A. 1971: Extension of Emmons' spot theory to flows on blunt bodies. AIAA J. 9, 821–825

    Google Scholar 

  • Devasia, K J. 1974: A study of the effect of pressure gradients on transition in the boundary layer on a flat plate. Master of Eng. Dissertation, Dept. Aero. Eng., Ind. Inst. Sci.

  • Dhawan, S.; Narasimha, R. 1958: Some properties of boundary layer flow during the transition from laminar to turbulent motion. J. Fluid Mech. 3, 318–436

    Google Scholar 

  • Emmons, H. W. 1951: The laminar-turbulent transition in a boundary layer — Part I. J. Aero. Sci. 18, 490–498

    Google Scholar 

  • Gururani, G. 1972: Effect of a favourable pressure gradient on transition in the boundary layer on a flat plate. Master of Eng. Dissertation, Dept. Aero. Eng., Ind. Inst. Sci.

  • Narasimha, R. 1957: On the distribution of intermittency in the transition region of a boundary layer. J. Aero. Sci. 24, 711–712

    Google Scholar 

  • Narasimha, R. 1958: A study of transition from laminar to turbulent flow in the boundary layer of a flat plate. Thesis for the Associateship of the Indian Institute of Science, Dept. Aero. Eng., Ind. Inst. Sci.

  • Narasimha, R. 1983: Laminar-turbulent transition: The intermittency revisited. Invited general lecture at 2nd Asian Cong. Fluid Mech., Beijing, October 1983. Also Report 83 FM 5, Dept. Aero. Eng., Ind. Inst. Sci.

  • Prasad, S. N. 1973: Two studies in airfoil design. Master of Eng. Dissertation, Dept. Aero. Eng., Ind. Inst. Sci.

Download references

Author information

Authors and Affiliations

Authors

Additional information

Now with Indian Space Research Organization

Now with Indian Air Force

Rights and permissions

Reprints and permissions

About this article

Cite this article

Narasimha, R., Devasia, K.J., Gururani, G. et al. Transitional intermittency in boundary layers subjected to pressure gradient. Experiments in Fluids 2, 171–176 (1984). https://doi.org/10.1007/BF00571859

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF00571859

Keywords

Navigation