Skip to main content
Log in

Controlling supersonic boundary layer stability by means of distributed mass transfer through a porous wall

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

Abstract

The interaction between disturbances in a compressible boundary layer in the presence of distributed mass transfer (injection or suction) through a permeable porous wall is considered in the linear and nonlinear approximations (weakly nonlinear stability theory). The regimes of moderate and high supersonic velocities (Mach numbers M = 2 and 5.35) are studied. The boundary conditions for the disturbances on a permeable wall are derived with account for the gas compressibility in pores and the presence of a suction chamber. Maximum pore dimensions, at which the surface properties have no effect on the disturbance characteristics, which are stabilized upon suction and destabilized upon injection, are determined. When the surface properties are taken into account, intense growth of the first-mode vortex disturbances occurs, which can completely undo the stabilizing effect of the suction. Injection leads to the vortex and acoustic mode destabilization on the linear range and the enhancement of the nonlinear processes on the transitional range.

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. H. Schlichting, Boundary Layer Theory, McGrow-Hill, New York (1968).

    Google Scholar 

  2. A.V. Boiko, G.R. Grek, A.V. Dovgal’, and V.V. Kozlov, Turbulence Generation inWall Flows [in Russian], Nauka, Novosibirsk (1999).

    Google Scholar 

  3. S.A. Gaponov and A.A. Maslov, Development of Disturbances in Compressible Flows [in Russian], Nauka, Novosibirsk (1980).

    Google Scholar 

  4. S.A. Gaponov and N.M. Terekhova, “Stability and Three-Wave Interaction between Disturbances in a Supersonic Boundary Layer with Mass Transfer on the Wall,” Teplofiz. Aeromekh. 19, 301 (2012).

    Google Scholar 

  5. S.A. Gaponov, N.M. Terekhova, and B.V. Smorodskii, “Three-Wave Interactions between Disturbances in a Hypersonic Boundary Layer,” Vestn. Novosib. Gos. Un-ta. Ser. Fizika 3(2), 39 (2008).

    Google Scholar 

  6. S.A. Gaponov and N.M. Terekhova, “Three-Wave Interactions between Disturbances in the Hypersonic Boundary Layer on Impermeable and Porous Surfaces,” Fluid Dynamics 44(3), 362 (2009).

    Article  ADS  MATH  MathSciNet  Google Scholar 

  7. S.A. Gaponov and N.M. Terekhova, “Linear Evolution and Interaction of Disturbances in the Compressible Boundary Layers on Impermeable and Porous Surfaces in the Presence of Heat Transfer,” Fluid Dynamics 46(3), 399 (2011).

    Article  ADS  MATH  MathSciNet  Google Scholar 

  8. S.A. Gaponov and B.V. Smorodsky, “Linear Stability of Supersonic Boundary Layer on Porous Surface,” in: Recent Advances in Fluid Mechanics and Aerodynamics, World Scientific and Engineering Academy and Society, Moscow (2009), p. 68.

    Google Scholar 

  9. D.A. Bountin, A.N. Shiplyuk, A.A. Maslov, and N. Chokani, “Nonlinear Aspects of Hypersonic Boundary Layer Stability on a Porous Surface,” in: 42nd AIAA Aerospace Sci. Meeting and Exhibition, Reno, NV. 2004 (2004).

    Google Scholar 

  10. S.A. Gaponov, Yu.G. Ermolaev, A.D. Kosinov, V.I. Lysenko, N.V. Semenov, and B.V. Smorodskii, “Effect of the Porous Coating Depth on the Stability and Transition of a Supersonic Flat-Plate Boundary Layer,” Teplofiz. Aeromekh. 19, 555 (2012).

    Google Scholar 

  11. Yu.S. Kachanov, “Physical Mechanisms of Laminar-Boundary-Layer Transition,” Annu. Rev. Fluid Mech. 26, 411 (1994).

    Article  ADS  MathSciNet  Google Scholar 

  12. M.B. Zel’man, “Nonlinear Development of Disturbances in Plane-Parallel Flows,” Izv. Sib. Otd. Akad. Nauk SSSR. Ser. Tekhn. Nauk No. 13(3), 16 (1974).

    Google Scholar 

  13. S.A. Gaponov and I.I. Maslennikova, “Subharmonic Instability of a Supersonic Boundary Layer,” Teplofiz. Aeromekh. 4, 1 (1997).

    Google Scholar 

  14. S.A. Gaponov and N.M. Terekhova, “Evolution of High-Intensity Disturbances in a Supersonic Boundary Layer,” Aeromekh. Gaz. Din. No. 1, 28 (2003).

    Google Scholar 

  15. F.B. Daniels, “On the Propagation of Sound Waves in a Cylindrical Conduit,” J. Acoust. Soc. Amer. 22, 563 (1950).

    Article  ADS  Google Scholar 

  16. S.A. Gaponov, “Effect of the Properties of a Porous Coating on the Boundary Layer Stability,” Izv. Sib. Otd. Akad. Nauk SSSR. Ser. Tekhn. Nauk No. 3(1), 21 (1971).

    Google Scholar 

  17. S.A. Gaponov, “Gas Compressibility Effect on the Stability of the Boundary Layer over a Permeable Surface at Subsonic Velocities,” Zh. Prikl. Mekh. Tekhn. Fiz. No. 1, 121 (1975).

    Google Scholar 

Download references

Authors

Additional information

Original Russian Text © S.A. Gaponov, N.M. Terekhova, 2013, published in Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, 2013, Vol. 48, No. 6, pp. 59–71.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Gaponov, S.A., Terekhova, N.M. Controlling supersonic boundary layer stability by means of distributed mass transfer through a porous wall. Fluid Dyn 48, 761–772 (2013). https://doi.org/10.1134/S0015462813060070

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S0015462813060070

Keywords

Navigation