TIP CLEARANCE FLOW IN A LOW SPEED HIGHLY STAGGERED COMPRESSOR CASCADE
عنوان مقاله: TIP CLEARANCE FLOW IN A LOW SPEED HIGHLY STAGGERED COMPRESSOR CASCADE
شناسه ملی مقاله: ISME13_587
منتشر شده در سیزدهمین کنفرانس سالانه مهندسی مکانیک در سال 1384
شناسه ملی مقاله: ISME13_587
منتشر شده در سیزدهمین کنفرانس سالانه مهندسی مکانیک در سال 1384
مشخصات نویسندگان مقاله:
Beheshti - Ph.D. Candidate Center of Excellence in Energy Conversion, School of Mechanical Engineering Sharif University of Technology, Tehran-Iran
Ghorbanian - Associate Professor Center of Excellence in Energy Conversion, School of Mechanical Engineering Sharif University of Technology, Tehran-Iran
Farhanieh - Professor Center of Excellence in Energy Conversion, School of Mechanical Engineering Sharif University of Technology, Tehran-Iran
خلاصه مقاله:
Beheshti - Ph.D. Candidate Center of Excellence in Energy Conversion, School of Mechanical Engineering Sharif University of Technology, Tehran-Iran
Ghorbanian - Associate Professor Center of Excellence in Energy Conversion, School of Mechanical Engineering Sharif University of Technology, Tehran-Iran
Farhanieh - Professor Center of Excellence in Energy Conversion, School of Mechanical Engineering Sharif University of Technology, Tehran-Iran
To get a better understanding of the complex flowfield in axial flow compressors, a three-dimensional incompressible solver with κ-ε turbulence model and unstructured grid has been applied to a highly staggered compressor cascade including tip clearance. For a linear compressor cascade with GE rotor B, the flowfield and pressure distributions are studied and compared with available experimental and numerical data. The computations are used to describe the features of tip clearance flow and furthermore, the tip leakage vortex and the endwall region flow characteristics are discussed.
کلمات کلیدی: Tip clearance – Axial flow compressor – Tip leakage vortex – Highly staggered
صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/27192/