NUMERICAL MODELING OF WALL-INJECTED SCRAMJET EXPERIMENTS

被引：9

作者：

BRESCIANINI, CP

MORGAN, RG

机构：

[1] University of Queensland, Brisbane, QLD

来源：

JOURNAL OF PROPULSION AND POWER | 1993年 / 9卷 / 02期

基金：

美国国家航空航天局; 澳大利亚研究理事会;

关键词：

D O I：

10.2514/3.23605

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A wall-injected, hydrogen-fueled scramjet is modeled numerically using a parabolic Navier-Stokes computer code with a k-epsilon turbulence model and finite-rate chemistry. The numerical results are compared to experimental scramjet data taken in a shock tunnel and are found to be in reasonable agreement. At the conditions studied, the numerical results show that combustion in the scramjet is mainly mixing limited.

引用

页码：169 / 175

页数：7

共 19 条

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[9]

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[10]

MORGAN RG, 1986, 1086 U QUEENSL DEP M

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