Skip to main content
Log in

Effect of the boundary layer on the base pressure in a two-dimensional flow with a Mach number M = 5

  • Published:
Journal of Applied Mechanics and Technical Physics Aims and scope

Abstract

New data on the base pressure in a two-dimensional ow with a Mach number M = 5 are obtained for a wide range of variation of the normalized boundary-layer thickness in the flow-separation cross section. The test results are compared with Tanner’s theory, and a conclusion is made that this numerical model has to be corrected.

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. S. N. B. Murthy and J. R. Osborn, “Base flow phenomena with and without injection: Experimental results, theories, and bibliography,” in: Progress in Astronautics and Aeronautics, Vol. 40: Aerodynamics of Base Combustion, AIAA, Washington (1976).

    Google Scholar 

  2. A. I. Shvets and I. T. Shvets, Near-Wake Gas Dynamics [in Russian], Naukova Dumka, Kiev (1976).

    Google Scholar 

  3. L. V. Gogish and G. Yu. Stepanov, Turbulent Separated Flows [in Russian], Nauka, Moscow (1979).

    Google Scholar 

  4. L. V. Gogish and G. Yu. Stepanov, Separated and Cavitation Flows: Basic Properties and Numerical Models [in Russian], Nauka, Moscow (1990).

    Google Scholar 

  5. M. Tanner, “Boundary layer thickness and base pressure,” AIAA J., 23, No. 12, 1985–1989 (1985).

    Google Scholar 

  6. M. Tanner, “Steady base flows,” Prog. Aerospace Sci., 21, No. 2, 81–157 (1989).

    Article  Google Scholar 

  7. M. Tanner, “Base pressure in supersonic flow, further thoughts about a theory,” AIAA J., 30, No. 2, 565–566 (1991).

    Google Scholar 

  8. M. G. Ktalkherman, “Gas dynamics of gas-dynamic and chemical laser channels,” Doct. Dissertation in Tech. Sci., Novosibirsk (1998).

  9. M. G. Ktalkherman and V. M. Malkov, “Gas-dynamic laser nozzle-unit aerooptics,” J. Appl. Mech. Tech. Phys., 34, No. 6, 761–766 (1993).

    Article  Google Scholar 

  10. V. M. Malkov and M. G. Ktalkherman, “Some aspects of aerodynamics of GDL nozzle banks,” AIAA Paper No. 94-2447 (1994).

  11. F. R. Hama, “Experimental studied on the lip-shock,” AIAA J., 23, No. 2 (1968).

    Google Scholar 

  12. K. Oswatisch, Grundkagen des Gasdynamic, Springer-Verlag, New York (1976).

    Google Scholar 

  13. E. C. Magi and S. L. Gay, “Supersonic base pressure and lip-shock,” AIAA J., 26, No. 3, 370–372 (1987).

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Additional information

__________

Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 46, No. 3, pp. 23–28, May–June, 2005.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Ktalkherman, M.G., Malkov, V.M. Effect of the boundary layer on the base pressure in a two-dimensional flow with a Mach number M = 5. J Appl Mech Tech Phys 46, 324–328 (2005). https://doi.org/10.1007/s10808-005-0081-x

Download citation

  • Received:

  • Revised:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10808-005-0081-x

Key words

Navigation