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Effect of Wall Suction and Cooling on the Second Mode Instability

  • Conference paper
Book cover Instability and Transition

Part of the book series: ICASE/ NASA LaRC Series ((ICASE/NASA))

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Abstract

Compressible linear viscous stability theory is used to study the effect of combined wall suction and cooling on the second mode instability in a flat plate boundary layer. While wall cooling destabilizes the boundary layer, calculations at Mach 4.5 and 8 show that wall suction may be used to stabilize the boundary layer with respect to second mode (subsonic) instability.

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References

  1. Lees, L. and Lin, C. C., “Investigation of the Stability of the Laminar Boundary Layer in a Compressible Fluid”, NACA Technical Note No. 1115, 1946 (unpublished).

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Author information

Authors and Affiliations

  1. High Technology Corporation, Hampton, VA, 23666, USA

    M. R. Malik & A. A. Godil

Authors
  1. M. R. Malik
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  2. A. A. Godil
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Editor information

Editors and Affiliations

  1. Institute for Computer Applications in Science and Engineering (ICASE) ICASE, NASA Langley Research Center, 23665, Hampton, VA, USA

    M. Y. Hussaini  & R. G. Voigt  & 

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© 1990 Springer-Verlag New York Inc.

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Malik, M.R., Godil, A.A. (1990). Effect of Wall Suction and Cooling on the Second Mode Instability. In: Hussaini, M.Y., Voigt, R.G. (eds) Instability and Transition. ICASE/ NASA LaRC Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-3432-6_18

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  • DOI: https://doi.org/10.1007/978-1-4612-3432-6_18

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-0-387-97324-1

  • Online ISBN: 978-1-4612-3432-6

  • eBook Packages: Springer Book Archive

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