TAYLOR-GOERTLER INSTABILITY OF COMPRESSIBLE BOUNDARY LAYERS.

Ryoji Kobayash, Yasuaki Kohama

    Research output: Contribution to journalArticle

    16 Citations (Scopus)

    Abstract

    The paper examines analytically how compressibility of a fluid will affect the instability of laminar boundary layers along slightly concave walls leading to the onset of longitudinal vortices. Neutral stability curves representing the relation of the Goertler parameter to the dimensionless wavenumber of the longitudinal vortices and also distributions of the disturbances at the onset of the vortices are presented. The results show that the critical value of the Goertler parameter increases about 1. 6 times as the freestream Mach number varies from 0 to 5 in the case of a thermally insulated wall. Effects of temperature ratio (wall temperature to freestream temperature) in cases of an isothermal wall are also discussed.

    Original languageEnglish
    Pages (from-to)1723-1727
    Number of pages5
    JournalAIAA Journal
    Volume15
    Issue number12
    Publication statusPublished - 1977 Dec

    ASJC Scopus subject areas

    • Aerospace Engineering

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  • Cite this

    Kobayash, R., & Kohama, Y. (1977). TAYLOR-GOERTLER INSTABILITY OF COMPRESSIBLE BOUNDARY LAYERS. AIAA Journal, 15(12), 1723-1727.