固体火箭技术Issue(3)：315-319,5.DOI:10.7673/j.issn.1006-2793.2014.03.006
面向总体设计的超燃冲压发动机空气流量
Design-oriented research of air mass flux characteristic for scramjet
摘要
Abstract
With regard to air mass flux characteristic of scramjet for airbreathing hypersonic flight vehicle,mathematical model of design-oriented air mass flux characteristic was derived by means of force analysis,energy conservation principle,specific impulse definition and so on.What’s more,design-oriented air mass flux characteristic was contrasted and analyzed in combination with in-stance in terms of quantitative and qualitative analysis.The results show that air mass flux obviously decreases by making use of hy-drocarbon fuel and air launch.Variation trend of cruising range was contrary to that of cruising speed,which requires optimization a-bout the both parameters.Air overflow and appropriate equivalent specific fuel consumption were required with mass reduction during cruise flight.关键词
空气流量/超燃冲压发动机/碳氢燃料/空中发射/航程/巡航速度Key words
air mass flux/scramjet/hydrocarbon fuel/air launch/cruising range/cruising speed分类
航空航天引用本文复制引用
田宪科,唐硕,田宪长..面向总体设计的超燃冲压发动机空气流量[J].固体火箭技术,2014,(3):315-319,5.基金项目
航天技术支撑基金（2013-HT-XGD-014）。 （）
