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Axisymmetric impingement of a hot jet on a flat plate: equilibrium flow analysis of high-temperature air
Authors:K. -H. Kim  K. -S. Chang
Affiliation:(1) Hyundai Motor Company, Korea;(2) Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Kusong-dong 373-1, Yusung-gu, 305-701 Taejon, Korea
Abstract:The flow structure of an underexpanded supersonic jet with high reservoir temperature impinging on a flat plate has been numerically investigated using a Total Variation Diminishing (TVD) scheme. When the temperature of the flow field is high enough to cause chemical reaction, the specific heat ratio,gamma, is no longer equal to 1.4, nor constant. This explains the difference found in the literature between the flow properties of the calorically perfect gas and that of the chemically reacting flow. Under the equilibrium flow assumption the effect of high temperature gas on the impinging jet has been taken into account in the present paper by using specific heat ratio and speed of sound given by correlation polynomials of thermodynamic variables. The limiting case of cold jet calculation in the present numerical results agreed well with the existing experimental data. For the equilibrium jet with high reservoir temperature,To=1000K, qualitative support of the present result has been provided by means of the approximation theory.This article was processed using Springer-Verlag TEX Shock Waves macro package 1.0 and the AMS fonts, developed by the American Mathematical Society.
Keywords:High-temperature equilibrium flow  Real gas effect  Shock wave structures  TVD numerical simulation  Underexpanded supersonic jet
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