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首页> 外文期刊>Journal of Propulsion and Power >Experimental Study of Vitiation Effects on Scramjet Mode Transition
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Experimental Study of Vitiation Effects on Scramjet Mode Transition

机译:通风对超燃冲压发动机模式转变的影响的实验研究

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MANY ground test facilities for studying dual-mode scramjetn(DMSJ) propulsion rely on stagnation enthalpy simulation viancombustion of hydrogen or hydrocarbon fuel. This heating processnresults in levels of vitiates in the test flow, such as water and carbonndioxide, that are not present in atmospheric air. The effects of thesenvitiates on DMSJ performance and operability must therefore benunderstood if accurate extrapolations to flight can be made. ThenSupersonic Combustion Facility [1] provides a unique opportunity tonstudy such effects since the facility is electrically heated and suppliesna test gas that is free of combustion generated vitiates. However,nwater vapor, in the form of steam, and carbon dioxide can be added tonthe flow to examine the effects these vitiates have on a DMSJ.nPrevious work to study vitiation effects has been performed using upnto 7% H2O and 2.5% CO2, both by mole [1]. However, these resultsnwere only obtained over a limited range of fuel equivalence ratios andnthe study did not fully investigate mode-transition with anprecombustion shock train due to the lack of a flowpath isolator.nThe present study was conducted with vitiate levels closer to thosenencountered in combustion heated facilities and with an isolatorninstalled. Reference [2] provides details of the new configuration.nBasically it consists of the DMSJ of [1], a rectangular, direct connectncombustor with a single ramp fuel injector, and a new constant area,nrectangular isolator that is ten duct heights long. This Note reports onnexperimental pressure measurements in the scramjet combustor atntwo vitiated conditions and compares the results with that of clean air.nWater and carbon dioxide levels are examined such that the effects ofnwater vapor vitiation can be isolated for conditions that are representativenof a methane combustion heated facility operating at Mach 5nsimulation. Trends in the data are examined, particularly with respectnto the effect vitiates have on the mode-transition characteristics ofnthe DMSJ.
机译:用于研究双模超燃冲压发动机(DMSJ)推进力的许多地面测试设施都依赖于氢或碳氢化合物燃料的停滞焓模拟燃烧。这种加热过程会导致测试流中的水分含量升高,例如水和二氧化碳,这是大气中不存在的。因此,如果可以对飞行进行准确的推断,就必须理解这些保护剂对DMSJ性能和可操作性的影响。然后,超音速燃烧设施[1]提供了一个独特的机会来研究这种效应,因为该设施是电加热的,并且供应没有燃烧产生的烟气的测试气体。但是,可以在水流中添加水蒸气(以蒸汽形式)和二氧化碳,以检查这些氧化物对DMSJ的影响。n以前的研究悬浮作用的研究是使用高达7%的H2O和2.5%的CO2进行的摩尔[1]。然而,这些结果仅在有限的燃料当量比范围内获得,并且由于缺少流路隔离器,因此本研究并未对带有预燃烧冲击波的模式转换进行充分研究。设施并安装了隔离器。参考文献[2]提供了新配置的详细信息。n它基本上由[1]的DMSJ组成,具有一个单斜坡燃油喷射器的矩形直接连接燃烧室,以及一个新的恒定面积的矩形隔离器,该隔离器的长度为十个管道高度。本说明报告了在两种通风条件下超燃冲压燃烧器中的实验压力测量结果,并将结果与​​清洁空气进行了比较.n检查了水和二氧化碳的含量,以便可以分离出代表甲烷燃烧加热设施的水蒸汽悬浮作用以5马赫的速度运行。检查了数据趋势,特别是关于振动对DMSJ的模式转换特性的影响。

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