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A Model for Adiabatic Supersonic Turbulent Boundary Layers (1996)

He, J. ; Kazakia, J. Y. ; Ruban, A. I. ; [et al.]

Springer

Theoretical and computational fluid dynamics 8 (1996), S. 349-364

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ISSN: 1432-2250

Source: Springer Online Journal Archives 1860-2000

Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics

Notes: Abstract An asymptotic analysis of the equations describing supersonic turbulent flow over an adiabatic wall is carried out for high Reynolds numbers, Re, and mainstream Mach numbers, A general expression for the adiabatic-wall temperature is derived. The asymptotic theory constrains the types of turbulence models that are suitable to represent the effects of viscous dissipation. A simple algebraic turbulence model is proposed and comparisons with measured total enthalpy profile data show good agreement, capturing the overshoot observed in total enthalpy near the boundary-layer edge.

Type of Medium: Electronic Resource

URL: http://dx.doi.org/10.1007/BF00456375

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