Effect of fence on linear aerospike plume-induced base-heating physics

被引:5
|
作者
Wang, TS [1 ]
机构
[1] NASA, George C Marshall Space Flight Ctr, Appl Fluid Dynam Anal Grp, Huntsville, AL 35812 USA
关键词
D O I
10.2514/2.6553
中图分类号
O414.1 [热力学];
学科分类号
摘要
A computational heat transfer analysis is conducted to study the effect of the presence of an engine fence on the X-33 linear aerospike plume-induced base heating during vehicle ascent. A fence is an extension of the plug side wall that reduces the plume spillage. A detailed three-dimensional thermoflowfield of the entire vehicle is computed such that an accurate freestream Row environment is assured for the base-dow development. The computational methodology is based on a finite difference, viscous flow, chemically reacting, pressure-based computational fluid dynamics formulation and a finite volume, spectral-line-based weighted sum of gray gases absorption computational radiation heat transfer formulation. The computed base-flow physics are analyzed and compared with those of a subscale model hot-flow test. The effect of base bleed is also analyzed.
引用
收藏
页码:457 / 463
页数:7
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