Upper bounds on the flight speed of hydrocarbon-fueled scramjet-powered vehicles

被引：22
|
作者：
Waltrup, PJ [1 ]
机构：
[1] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD 20723 USA
来源：
JOURNAL OF PROPULSION AND POWER | 2001年 / 17卷 / 06期
关键词：
Flight dynamics - Hydrocarbons - Liquid fuels - Missiles - Nozzles - Supersonic aerodynamics;
D O I：
10.2514/2.5895
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Estimates of upper bounds on flight Mach number for scramjet-powered vehicles operating on liquid hydrocarbon fuels assuming either equilibrium or frozen nozzle chemistry are presented. For an axisymmetric: missile-shaped vehicle, these upper bounds lie between Mach 9 and 10.
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页码：1199 / 1204
页数：6
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