Performance of a miniature gas turbine engine

被引：0
|
作者：
Ho, WC
Liu, CP
Weng, LC
Liu, MY
Wey, TW
机构：
来源：
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 1996年 / 13卷 / 01期
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D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The performance of a miniature gas turbojet engine for powering an aircraft is investigated experimentally. The engine is fueled by propane gas to avoid the difficulty of atomization, evaporation, and combustion of the liquid fuel in a small combustor. The operating characteristics of the engine are attained through measurements of temperature, pressure, thrust, volumetric flowrate of air, fuel and lubricant consumption rates, rotation speed of shaft, and exhaust gas composition.
引用
收藏
页码：65 / 68
页数：4
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