Skip to main content
Log in

Analysis of interactions between shock waves and laminar boundary layers with heat transfer

  • Continued from Outside
  • Published:
Acta Mechanica Aims and scope Submit manuscript

Summary

This paper deals with interactions between shock waves and laminar boundary layers on flat plates with heat transfer. In order to describe this phenomenon the boundary layer is divided into inner viscous layer and outer inviscid layer after Gadd. The boundary layer approximations are assumed to remain valid in the inner layer and the momentum integral equation for the layer is utilized instead of the Pohlhausen's wall condition. In the outer inviscid layer the motion is described by Euler's equation in terms of the isobar coordinates and the deflection angle is determined to match with that at the outer edge of the inner layer. The present theory predicts that self-induced separation does occur for highly cooled wall and yields results in good agreement with the measurement of Lewis et al.

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. Stewartson, K.: Multistructured boundary layers on flat plates and related bodies. Advances in Applied Mechanics Vol.14, p. 145, New York: Academic Press 1974.

    Google Scholar 

  2. Adamson, T. C., Messiter, A. F.: Analysis of two-dimensional interactions between shock waves and boundary layers. Annual Review of Fluid Mech. Vol.12, p. 103, Palo Alto: Annual Review 1980.

    Google Scholar 

  3. Lees, L., Reeves, B. L.: Supersonic separated and, reattaching laminar flows: I. General theory and application to adiabatic boundary-layer/shock-wave interactions. AIAA J.2, 1907–1920 (1964).

    Google Scholar 

  4. Nielsen, J. N., Lynes, L. L., Goodwin, F. K.: Theory of laminar separated flows on flared surfaces including supersonic flow with heating and cooling, AGARD Conf. Proc. no 4, pp. 31–68 (Separated Flows), 1966.

    Google Scholar 

  5. Klineberg, J. M., Lees, L.: Theory of laminar viscous-inviscid interactions in supersonic flow. AIAA J.7, 2211–2221 (1969).

    Google Scholar 

  6. Gadd, G. E.: A theoretical investigation of laminar separation in supersonic flow. J. Aeronautical Sci.24, 759–771, 784 (1957).

    Google Scholar 

  7. Lighthill, M. J.: On boundary layers and upstream influence II. Supersonic flows without separation. Proc. Roy. Soc. LondonA 217, 478–507 (1953).

    Google Scholar 

  8. Stewartson, K., Williams, P. G.: Self-induced separation. Proc. Roy. Soc. LondonA 312, 181–206 (1969).

    Google Scholar 

  9. Нейланд, В. Я: К теории отрива ламинарного пограничного слоя в сверхзвуковом Изв. AH CCCP Механика Жидкости и Газа, No.4, 53–57 (1969).

    Google Scholar 

  10. Нейланд, В. Я.: Осоьенности отрыва пораничного слоя на охлаждаемом теле и его взаимодействие с гиперзвуковым потоком. Изв. AH CCCP Механика жидкости и Газа, No. 6, 99–109 (1973).

    Google Scholar 

  11. Stewartson, K.: Theory of laminar boundary layers in compressible fluids, p. 61. Oxford University Press 1964.

  12. Honda, M., Igarashi, S.: Analysis of the boundary-layer flow under a steep pressure rise, Part 1. Laminar flow. Rep. Inst. High Speed Mech., Tohoku Univ.,40, 51–68 (1969).

    Google Scholar 

  13. Honda, M.: Stream-function co-ordinates in rotational flow and an analysis of the flow in a shock layer, I. Two-dimensional flow. J. Inst. Maths Applics,1, 127–148 (1965).

    Google Scholar 

  14. Lewis, J. E., Kubota, T., Lees, L.: Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling. AIAA J.6, 7–14 (1968).

    Google Scholar 

  15. Gadd, G. E.: An experimental investigation of heat transfer effects on boundary layer separation in supersonic flow. J. Fluid Mech.2, 105–122 (1957).

    Google Scholar 

  16. Hakkinen, R. J., Greber, I., Trilling, L., Abarbanel, S. S.: The interaction of an oblique shock wave with a laminar boundary layer. NASA Memo. 2-18-59W (1959).

Download references

Author information

Authors and Affiliations

Authors

Additional information

With 6 Figures

Rights and permissions

Reprints and permissions

About this article

Cite this article

Igarashi, S., Honda, M. & Onodera, K. Analysis of interactions between shock waves and laminar boundary layers with heat transfer. Acta Mechanica 73, 221–230 (1988). https://doi.org/10.1007/BF01177041

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01177041

Keywords

Navigation