Laminar Base Flow Downstream of Slender Cones in Hypersonic Flow

被引：4
|
作者：
Gorshkov, A. B.
Lunev, V. V.
机构：
来源：
FLUID DYNAMICS | 2002年 / 37卷 / 05期
基金：
俄罗斯基础研究基金会;
关键词：
hypersonic flow; heat transfer; cone; base flow; numerical simulation;
D O I：
10.1023/A:1021380605136
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The base flow downstream of slender cones in a stream of perfect gas at Mach numbers 8 and 10 and Reynolds numbers 10(4) and 10(5) is numerically investigated. The calculated heat fluxes to the rear face of the body are compared with experimental data. It is shown that the friction and heat transfer coefficients increase without bound as the corner point is approached from both the lateral surface and the rear face, the sign of the latter coefficient being dependent on the body surface temperature factor.
引用
收藏
页码：772 / 783
页数：12
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