دورية أكاديمية

Numerical Study on End Wall Synthetic Jet to Improve Performance and Stability Margin of a High-speed Subsonic Axial Compressor Rotor

التفاصيل البيبلوغرافية
العنوان: Numerical Study on End Wall Synthetic Jet to Improve Performance and Stability Margin of a High-speed Subsonic Axial Compressor Rotor
المؤلفون: G. Wang, W. Chu, W. Liu
المصدر: Journal of Applied Fluid Mechanics, Vol 16, Iss 6, Pp 1269-1280 (2023)
بيانات النشر: Isfahan University of Technology, 2023.
سنة النشر: 2023
المجموعة: LCC:Mechanical engineering and machinery
مصطلحات موضوعية: compressor, end wall, synthetic jet, performance improvement, numerical simulation, Mechanical engineering and machinery, TJ1-1570
الوصف: Synthetic jet has been confirmed as a novel flow control technology. However, the existing application research on synthetic jet in axial flow compressor is still confined to cascade or low-speed axial flow compressors, and rarely high-speed axial flow compressor. The effects of three vital parameters (i.e., the action position, frequency, peak velocity) on the aerodynamic performance and stability margin are systematically studied, with a high-speed compressor rotor as the object of numerical simulation. An optimal excitation position is determined, corresponding to the core position of the compressor top blockage, as indicated by the results, which increases the stability margin and efficiency of the compressor by 13.2% and 1.15% respectively. The excitation frequency has a threshold ranging from 300Hz to 600Hz. Only when the frequency of synthetic jet exceeds this threshold can it suppress the tip leakage flow. Besides, the jet peak velocity may not have a threshold. However, the higher the peak velocity, the greater the mixing loss between the jet and the mainstream of the compressor rotor will be, thus limiting the further increase of the compressor efficiency.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 1735-3572
1735-3645
Relation: https://www.jafmonline.net/article_2222_c12da02acf89a55f8d1d396c3e0baf68.pdf; https://doaj.org/toc/1735-3572; https://doaj.org/toc/1735-3645
DOI: 10.47176/jafm.16.06.1587
URL الوصول: https://doaj.org/article/11dd533ea7c9413eb2b34438dfbeaba0
رقم الأكسشن: edsdoj.11dd533ea7c9413eb2b34438dfbeaba0
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:17353572
17353645
DOI:10.47176/jafm.16.06.1587