COMBUSTION CHARACTERISTICS OF A BORON-FUELED SOLID-FUEL RAMJET WITH AFT-BURNER

被引：28
|
作者：
NATAN, B
GANY, A
机构：
[1] Israel Institute of Technology, Haifa
来源：
JOURNAL OF PROPULSION AND POWER | 1993年 / 9卷 / 05期
关键词：
D O I：
10.2514/3.23677
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The research deals with a theoretical evaluation of the concept of using an afterburner in a solid fuel ramjet motor, where bypass air is added, as a means of enhancing combustion efficiencies of boron containing fuels. A theoretical model is developed and solved numerically. A parametric investigation examines the effect of pressure, air mass flux, equivalence ratio, inlet air temperature, and the aft-burner length. The results reveal that good boron combustion efficiencies and high temperatures can be obtained at optimal conditions.
引用
收藏
页码：694 / 701
页数：8
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