Numerical investigation of supersonic viscous gas flow over long blunt cones with allowance for equilibrium physicochemical effects

S. V. Utyuzhnikov

doi:10.1007/BF01055681

Numerical investigation of supersonic viscous gas flow over long blunt cones with allowance for equilibrium physicochemical effects

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Abstract

Supersonic axisymmetric viscous heat-conducting gas flow over long spherically biunted cones is considered over a broad range of Reynolds numbers on the basis of the complete system of viscous shock layer equations. An economical numerical method based on global iterations is used to solve the viscous shock layer equations. The general influence of the second-approximation effects of boundary layer theory and the influence of equilibrium physicochemical processes on the heat loads are determined for bodies with a large aspect ratio. © 1993 Plenum Publishing Corporation.

Original language	English
Pages (from-to)	155-158
Number of pages	3
Journal	Fluid Dynamics
Volume	28
Issue number	1
DOIs	https://doi.org/10.1007/BF01055681
Publication status	Published - Jan 1993

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title = "Numerical investigation of supersonic viscous gas flow over long blunt cones with allowance for equilibrium physicochemical effects",

abstract = "Supersonic axisymmetric viscous heat-conducting gas flow over long spherically biunted cones is considered over a broad range of Reynolds numbers on the basis of the complete system of viscous shock layer equations. An economical numerical method based on global iterations is used to solve the viscous shock layer equations. The general influence of the second-approximation effects of boundary layer theory and the influence of equilibrium physicochemical processes on the heat loads are determined for bodies with a large aspect ratio. {\textcopyright} 1993 Plenum Publishing Corporation.",

author = "Utyuzhnikov, {S. V.}",

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AB - Supersonic axisymmetric viscous heat-conducting gas flow over long spherically biunted cones is considered over a broad range of Reynolds numbers on the basis of the complete system of viscous shock layer equations. An economical numerical method based on global iterations is used to solve the viscous shock layer equations. The general influence of the second-approximation effects of boundary layer theory and the influence of equilibrium physicochemical processes on the heat loads are determined for bodies with a large aspect ratio. © 1993 Plenum Publishing Corporation.

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DO - 10.1007/BF01055681

M3 - Article

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JO - Fluid Dynamics

JF - Fluid Dynamics

IS - 1

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Numerical investigation of supersonic viscous gas flow over long blunt cones with allowance for equilibrium physicochemical effects

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