涡轮喷气发动机燃烧室特性研究

IF 0.8 Q3 ENGINEERING, AEROSPACE

Aviation Pub Date : 2021-04-16 DOI:10.3846/AVIATION.2021.14398

Andrius Dubovas, D. Bručas

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引用次数: 0

摘要

本文研究了不同参数下涡轮喷气发动机燃烧室的特性。回顾了其他作者分析喷气发动机工作参数的科学工作。审议了他们的建议。采用不同的燃烧反应对燃烧室进行了计算机模拟。测定了排气温度及其与燃烧混合气的关系。并进行了实际研究，测量了实验废气温度，确定了温度变化趋势。通过对理论和实践结果的分析，得出了结论。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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RESEARCH ON CHARACTERISTICS OF TURBO JET ENGINE COMBUSTION CHAMBER

The characteristics of the combustion chamber of turbo jet engine with various parameters are examined in this article. The scientific works of other authors analyzing operating parameters of the jet engines were reviewed. Their recommendations were considered. Computer simulations of the combustion chamber were performed using different combustion reactions. The exhaust gas temperature and its dependence on the combustion mixture were determined. A practical study was also carried out, during which the experimental exhaust gas temperature was measured, and the trends of temperature change were determined. After analyzing both theoretical and practical results, the conclusions are presented.

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来源期刊

Aviation ENGINEERING, AEROSPACE-

CiteScore

2.40

自引率

10.00%

发文量

审稿时长

15 weeks

期刊介绍： CONCERNING THE FOLLOWING FIELDS OF RESEARCH: ▪ Flight Physics ▪ Air Traffic Management ▪ Aerostructures ▪ Airports ▪ Propulsion ▪ Human Factors ▪ Aircraft Avionics, Systems and Equipment ▪ Air Transport Technologies and Development ▪ Flight Mechanics ▪ History of Aviation ▪ Integrated Design and Validation (method and tools) Besides, it publishes: short reports and notes, reviews, reports about conferences and workshops