{"title":"基于集成推进系统的通用超燃冲压发动机整体特性估算方法研究","authors":"R. Seleznev","doi":"10.33257/phchgd.24.1.1017","DOIUrl":null,"url":null,"abstract":"This paper describes the method for estimating the integral characteristics of a generic scramjet with an integrated pro-pulsion system. Calculations of the specific impulse and heat fluxes in the propulsion system for the X-43 and X-51 generic scramjets have been carried out. The results obtained are in good agreement with the estimates of other authors (in the speed range 5 < M < 10), as well as with the known graphs of the dependence of the specific impulse for various types of engines depending on the flight Mach number","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"160 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"On the Method for Estimating the Integral Characteristics of a Generic Scramjet with an Integrated Propulsion System\",\"authors\":\"R. Seleznev\",\"doi\":\"10.33257/phchgd.24.1.1017\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes the method for estimating the integral characteristics of a generic scramjet with an integrated pro-pulsion system. Calculations of the specific impulse and heat fluxes in the propulsion system for the X-43 and X-51 generic scramjets have been carried out. The results obtained are in good agreement with the estimates of other authors (in the speed range 5 < M < 10), as well as with the known graphs of the dependence of the specific impulse for various types of engines depending on the flight Mach number\",\"PeriodicalId\":309290,\"journal\":{\"name\":\"Physical-Chemical Kinetics in Gas Dynamics\",\"volume\":\"160 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Physical-Chemical Kinetics in Gas Dynamics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.33257/phchgd.24.1.1017\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Physical-Chemical Kinetics in Gas Dynamics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.33257/phchgd.24.1.1017","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
摘要
本文介绍了一种综合推进系统的通用超燃冲压发动机整体特性的估算方法。对X-43和X-51型超燃冲压发动机推进系统的比冲和热流进行了计算。所得到的结果与其他作者的估计(在速度范围5 < M < 10)以及与已知的各种类型的发动机的比冲依赖于飞行马赫数的曲线图很好地一致
On the Method for Estimating the Integral Characteristics of a Generic Scramjet with an Integrated Propulsion System
This paper describes the method for estimating the integral characteristics of a generic scramjet with an integrated pro-pulsion system. Calculations of the specific impulse and heat fluxes in the propulsion system for the X-43 and X-51 generic scramjets have been carried out. The results obtained are in good agreement with the estimates of other authors (in the speed range 5 < M < 10), as well as with the known graphs of the dependence of the specific impulse for various types of engines depending on the flight Mach number
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