Mathematical Model of Turbojet Engine Combustion Chamber Primary Zone

被引：0

作者：

Davidovic, Nikola ^{[1
]}

机构：

[1] Univ Belgrade, Fac Mech Engn, Belgrade, Serbia

来源：

FME TRANSACTIONS | 2007年 / 35卷 / 01期

关键词：

combustion chamber; vaporizer; primary zone; turbojet;

D O I：

暂无

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

Mathematical model of turbojet engine primary zone was developed and tested. Combustion chamber was of annular type with single annular vaporizer positioned at the center. This configuration is very attractive for the applications where small dimensions are of primary interest. The model was tested as a part of combustion chamber and it was estimated through the overall combustion chamber efficiency.

引用

页码：29 / 34

页数：6

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