Modeling and Performance Prediction of a Combined Axial-RadialCompressor of a Gas Turbine Engine
سال انتشار: 1402
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 146
فایل این مقاله در 5 صفحه با فرمت PDF قابل دریافت می باشد
- صدور گواهی نمایه سازی
- من نویسنده این مقاله هستم
استخراج به نرم افزارهای پژوهشی:
شناسه ملی سند علمی:
AEROSPACE22_034
تاریخ نمایه سازی: 31 مرداد 1403
چکیده مقاله:
Axial and radial compressors are used in many industries, like power generation, transportation, etc. ۱D or mean line modeling and performance prediction of these important machines are of the main steps in the design procedure. In this research ۱D modeling and performance prediction of a combined axial and radial compressor is carried out. A general method is proposed for the mean line modeling of this compressor. To validate the modeling results, they are compared with experimental data of the operating baseline gas turbine engine and there is a good agreement with maximum ۴% difference.
کلیدواژه ها:
نویسندگان
Amin Anjomrouz
Mechanical Engineering Department,Sharif University of Technology, Tehran, Iran
Ali HajilouyBenisi
Mechanical Engineering Department,Sharif University of Technology, Tehran, Iran