Augmented Burnett-equation solutions over axisymmetric blunt bodies in hypersonic flow
نویسندگان
چکیده
منابع مشابه
Augmented Burnett-Equation Solutions over Axisymmetric Blunt Bodies in Hypersonic Flow
We obtained augmented Burnett-equation solutions and conducted some preliminary studies on the extent to which the Burnett equations can be used in estimating the departure from the NavierStokes model for hypersonic flow over axisymmetric blunt bodies. The augmented Burnett equation solutions were restricted to the flow inside the bow shock in the stagnation region because of the uncertainty of...
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متن کاملapproximate viscous shock-layer analysis of axisymmetric bodies in perfect gas hypersonic flow
in this paper, an approximate axisymmetric method is developed which can reliably calculate fully viscous hypersonic flow over blunt-nosed bodies. in this method, a maslen’s second-order pressure expression is used instead of the normal momentum equation. the combination of maslen’s second-order pressure expression and viscous shock layer equations is developed to accurately and efficiently com...
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ژورنال
عنوان ژورنال: Journal of Spacecraft and Rockets
سال: 1995
ISSN: 0022-4650,1533-6794
DOI: 10.2514/3.26657