HIGHER-ORDER EFFECTS IN BOUNDARY-LAYER PREMIXED COMBUSTION

被引：3

作者：

TREVINO, C ^{[1
]}

STUTTGEN, W ^{[1
]}

PETERS, N ^{[1
]}

机构：

[1] INST TECH MECH,AACHEN,GERMANY

来源：

JOURNAL OF PROPULSION AND POWER | 1990年 / 6卷 / 03期

关键词：

D O I：

10.2514/3.25425

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Higher-order effects in the boundary-layer theory are included in the present analysis to evaluate the interaction of the expansion process from the premixed combustion of reacting gases with the potential flowTwo cases are considered: 1) the premixed combustion process, which takes place above the flat plate, and 2) the premixed flame, which is generated in the wake of the flat plate. In both cases, the strong expansion process, when interacting with the outer inviscid flow, produces relatively strong pressure gradients, modifying the aerodynamic structure of the flow. © 1988 American Institute of Aeronautics and Astronautics.

引用

页码：237 / 242

页数：6

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