Profiling of a Supersonic Combustion Chamber and Nozzle Under Constraints on the Total Length

被引：0
|
作者：
Kraiko, A.N.
Makarov, V.E.
Tillyayeya, N.I.
机构：
来源：
Fluid Dynamics | 1998年 / 33卷 / 05期
关键词：
Nozzles;
D O I：
暂无
中图分类号：
V43 [推进系统（发动机、推进器）]; V238 [];
学科分类号：
080703 ; 082502 ;
摘要：
A method of combined profiling of a combustion chamber and two-dimensional supersonic nozzle with a given total length is demonstrated with reference to a hydrogen/air hypersonic ramjet. The possibility of a considerable increase in thrust is illustrated by various devices designed within the framework of the method developed. © 1998, Plenum Publishing Corporation.
引用
收藏
页码：637 / 644
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