Determination of cycle configuration of gas turbines and aircraft engines by an optimization procedure

被引：0

作者：

Tsujikawa, Y. ^{[1
]}

Nagaoka, M. ^{[1
]}

机构：

[1] Univ Osaka Prefecture, Sakai, Japan

来源：

Journal of Engineering for Gas Turbines and Power | 1991年 / 113卷 / 01期

关键词：

Aero-Engine Specific Impulse - Gas Turbine Cycle Configuration - Multiplier Method - Ramjet Engine - Stationary Gas Turbine - Turbojet Engine Optimum Specific Thrust;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：100 / 105

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