燃烧加热污染空气对煤油超燃冲压发动机性能的影响  

Effects of combustion heating vitiated air on kerosene-fueled scramjet performance

作　　者：陈亮[1] 宋文艳[1] 罗飞腾[1] 刘昊[1] 李建平[1] 

机构地区：[1]西北工业大学动力与能源学院,西安710072

出　　处：《航空动力学报》2013年第11期2408-2418,共11页Journal of Aerospace Power

基　　金：西北工业大学科技创新基金(2012KJ01004)

摘　　要：针对目前超燃冲压发动机地面试验设备普遍存在的工质污染问题,采用经过验证的数值计算方法开展了燃烧加热污染空气对煤油超燃冲压发动机性能的影响研究.以飞行马赫数为6.0作为基准状态,分别对纯净空气来流和不同参数匹配方案的污染空气来流下发动机整机流场和性能进行了数值模拟.计算结果表明:在压力参数中选择匹配静压时最接近于纯净空气来流的结果,选择匹配总压时差别最大;在温度参数中选择匹配静温时最接近于纯净空气来流的结果,选择匹配总温时差别最大;压力参数匹配选择的影响更具有决定性作用,需要优先考虑.研究结果可为认识整机污染效应影响,确定污染空气来流下地面试验模拟准则提供理论依据.For the problem of test media vitiation associated with scramjet ground test facility, the effects of combustion heating vitiated air on kerosenefueled scramjet perform ance were investigated with validated numerical approach. Under the simulating condition of flight Mach 6.0, the flowfield and performance of the scramjet were numerically calculated with clean free airstream and vitiated free airstream, respectively. Several matched parame ter schemes for vitiated free airstream relative to clean air were considered. It indicates that among the pressureinterrelated parameters, the least discrepancy resulting from vitiation effects is found when the static pressure is matched, while the most discrepancy is found when the total pressure is matched; among the temperatureinterrelated parameters, the least discrepancy resulting from vitiation effects is found when the static temperature is matched, while the most discrepancy is found when the total temperature is matched. As for the vitiation effects of combustion heating vitiated air, selection of pressureinterrelated pa rameters to be matched is more significant than selection of temperatureinterrelated parame ters. The present efforts can provide theoretical basis for understanding the vitiation effects on the scramjet and determining the simulation rules of ground test with vitiated free airstream.

关 键 词：超燃冲压发动机 煤油燃料 燃烧加热 污染效应 数值计算 

分 类 号：V235.211[航空宇航科学与技术—航空宇航推进理论与工程]