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Advanced Simulation Technologies And Testing Methodologies Applied In The Design And Development Of Aero Gas Turbine Engines

机译:先进的仿真技术和测试方法在航空涡轮发动机的设计和开发中的应用

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摘要

An overview of Gas Turbine Engine Development, KAVERI, the power plant for the Light Combat Aircraft (Tejas) and a description of the validated numerical tools, aerothermody-namic and mechanical test facilities of the Gas Turbine Research Establishment (GTRE) are presented. The KA VERI engine compressor, combustion system, turbine, analytical tools, blade heat transfer, exhaust system, Integrated Nozzle Actuation System (INAS), Non-intrusive Stress Measurement System (NSMS) and thermal paint tests are described in detail.
机译:概述了燃气涡轮发动机的发展,KAVERI,轻型战斗机(Tejas)的动力装置,并对燃气涡轮研究机构(GTRE)的经过验证的数值工具,航空热力学和机械测试设施进行了描述。详细描述了KA VERI发动机压缩机,燃烧系统,涡轮机,分析工具,叶片传热,排气系统,集成喷嘴致动系统(INAS),非侵入式应力测量系统(NSMS)和热喷涂测试。

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