Optimum contour of aerospike nozzle

被引：0
|
作者：
Dai, Wu-ye [1 ]
Liu, Yu [1 ]
机构：
[1] Beijing Univ of Aeronautics and, Astronautics, Beijing, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2000年 / 21卷 / 05期
关键词：
Calculations - Mathematical models - Nozzles - Optimization;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
To maximize the total impulse of aerospike nozzle engine, numerical computation method was adopted on the full travel contour optimization of aerospike nozzle. The process of building optimization model including the assumptions and the steps of the contour optimization was presented in detail. The typical results of contour optimum, which can be used for contour design of aerospike nozzle, were also shown.
引用
收藏
页码：26 / 30
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