The Effect of Cooling on the Supersonic Boundary Layer Stability and Transition

  • V. I. Lysenko
  • A. A. Maslov
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

Summary

The present paper describes the carried out experimental studies of the laminar boundary layer stability on a flat plate and the transition into a turbulent state both by cooling of a streamlined surface and by its heating. There are confirmed the main theses of the linear theory of hydrodynamic stability. An explanation of the transition reversal appearing in tests in the wind tunnels on cooled models is given.

Keywords

Vortex Crystallization Steam Tungsten Dinate 

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 1.
    Gaponov, S.A.; Maslov, A.A.: Disturbance propagation in compressible flows (in Russian). Novosibirsk: Nauka 1980.Google Scholar
  2. 2.
    Laufer, J.; Vrebalovich, T.: Stability and transition of a supersonic laminar boundary layer on an insulated flat plate. J. Fluid Mech. 9 (1960) 257–299.CrossRefMATHADSGoogle Scholar
  3. 3.
    Lebiga, V.A.; Maslov, A.A.; Pridanov, Y.G.: Experimental investigation of the stability of supersonic boundary layer on a flat insulated plate. Archives Mech. 31 (1979) N3, 397–405.Google Scholar
  4. 4.
    Mack, L.M.: Linear stability theory and the problem of supersonic boundary layer transition. AIAA Journal 13 (1975) N3, 278–289.CrossRefADSGoogle Scholar
  5. 5.
    Mack, L.M.: Boundary layer stability theory. Document 900–277, JPL, 1969.Google Scholar
  6. 6.
    Maslov, A.A.: Numerical investigation of the stability of the supersonic laminar boundary layer (in Russian). Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki (1972) N5, 181–184.Google Scholar
  7. 7.
    Demetriades, A.: New experiment on hypersonic boundary layer stability including wall temperature effects. Proceeding of the 1978 Heat Transfer and Fluid Mechanics Institute. Stanford University Press. (1978) 39–56.Google Scholar
  8. 8.
    Lysenko, V.I.; Maslov, A.A.: Transition of laminar supersonic boundary layer into turbulent one by surface cooling (in Russian). Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki (1981) N3, 30–36.Google Scholar
  9. 9.
    Lysenko, V.I.; Maslov, A.A.: Experimental study of the influence of heating on supersonic boundary layer transition and stability (in Russian). Izv. SO AN SSSR (1981) N13, 42–49.Google Scholar
  10. 10.
    Lysenko, V.I.; Maslov, A.A.: Transition reversal and one of its causes. AIAA Journal 19 (1981) N6, 705–708.CrossRefADSGoogle Scholar
  11. 11.
    Lysenko, V.I.; Maslov, A.A.: The effect of cooling on supersonic boundary-layer stability. J.Fluid Mech.(to appear).Google Scholar

Copyright information

© Springer-Verlag, Berlin, Heidelberg 1985

Authors and Affiliations

  • V. I. Lysenko
    • 1
  • A. A. Maslov
    • 1
  1. 1.Institute of Theoretical and Applied MechanicsUSSR Academy of SciencesNovosibirskUSSR

Personalised recommendations