脉冲管在高超声速飞机发动机试验中的应用

ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities Pub Date : 1995-07-18 DOI:10.1109/ICIASF.1995.519482

A. Latypov, M. I. Yaroslavtsev, V. Zudov

{"title":"脉冲管在高超声速飞机发动机试验中的应用","authors":"A. Latypov, M. I. Yaroslavtsev, V. Zudov","doi":"10.1109/ICIASF.1995.519482","DOIUrl":null,"url":null,"abstract":"At M/sub H/=10, 12.2; T/sub OH/=2400 K, P/sub OH/=300-400 MPa in the hot-short aerodynamic tunnel, investigations of operating processes in the engine path of the scramjet model were performed. The model has rather simple external configuration. The inner channels are those ones which allow the burning of gaseous hydrogen as in sub- and super-sonic flows. Quantitative data on the distribution of pressure in the engine path were obtained. The experiments were performed in the IT-302M wind tunnel.","PeriodicalId":339620,"journal":{"name":"ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities","volume":"496 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1995-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Application of pulse tube for the test of the engines of hypersonic aircraft\",\"authors\":\"A. Latypov, M. I. Yaroslavtsev, V. Zudov\",\"doi\":\"10.1109/ICIASF.1995.519482\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"At M/sub H/=10, 12.2; T/sub OH/=2400 K, P/sub OH/=300-400 MPa in the hot-short aerodynamic tunnel, investigations of operating processes in the engine path of the scramjet model were performed. The model has rather simple external configuration. The inner channels are those ones which allow the burning of gaseous hydrogen as in sub- and super-sonic flows. Quantitative data on the distribution of pressure in the engine path were obtained. The experiments were performed in the IT-302M wind tunnel.\",\"PeriodicalId\":339620,\"journal\":{\"name\":\"ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities\",\"volume\":\"496 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1995-07-18\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICIASF.1995.519482\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICIASF.1995.519482","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 2

摘要

M/sub H/=10时，12.2;T/sub OH/=2400 K, P/sub OH/=300-400 MPa，在热短气动通道中对超燃冲压发动机模型在发动机路径上的工作过程进行了研究。该模型具有相当简单的外部配置。内部通道是那些允许在亚音速和超音速流动中燃烧气态氢的通道。获得了发动机路径内压力分布的定量数据。实验在IT-302M风洞中进行。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Application of pulse tube for the test of the engines of hypersonic aircraft

At M/sub H/=10, 12.2; T/sub OH/=2400 K, P/sub OH/=300-400 MPa in the hot-short aerodynamic tunnel, investigations of operating processes in the engine path of the scramjet model were performed. The model has rather simple external configuration. The inner channels are those ones which allow the burning of gaseous hydrogen as in sub- and super-sonic flows. Quantitative data on the distribution of pressure in the engine path were obtained. The experiments were performed in the IT-302M wind tunnel.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities

自引率

0.00%

发文量