Numerical Study on Local Entropy Production Mechanism of a Contra-Rotating Fan

被引:0
作者
Jia, Xingyu [1 ]
Zhang, Xi [1 ]
机构
[1] China Univ Min & Technol Beijing, Sch Mech Elect & Informat Engn, Ding 11 Xueyuan Rd, Beijing 100083, Peoples R China
基金
中国国家自然科学基金;
关键词
contra-rotating fan; local entropy production; tip leakage flow; shear strain rate; optimal design of radial load; NEURAL-NETWORKS; OPTIMIZATION; VANE;
D O I
10.3390/e25091293
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
Contra-rotating fans (CRFs) have garnered significant attention due to their higher power-to-weight ratio compared to traditional fans; however, limited focus has been given to the localization and development of local aerodynamic losses. Furthermore, there is a need for further research on the impact of load distribution along the radius on local entropy production. Therefore, this study aims to investigate a contra-rotating fan as the research subject. An optimal design for load distribution along the radius is achieved by constructing a surrogate model in combination with a genetic algorithm. The effectiveness of this design has been verified through experimentation using a specific test device. In this study, a local entropy production rate (EPR) model adapted to the shear stress transport-detached eddy simulation (SST-DES) technique is constructed to evaluate the loss distribution of the contra-rotating fan. This paper primarily focuses on comparing and analyzing the blade profile and overall performance of the CRFs before and after optimization. The EPR contribution of each interval along the radius is compared to the corresponding blade channel to identify the approximate range of high-EPR regions. Furthermore, an investigation is conducted to examine the distribution of EPR along the streamwise direction in these high-EPR regions. After that, by comparing the development of the flow structure near a stall before and after optimization, combined with the analysis of the EPR contours, the EPR mechanism of this CRF is revealed.
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页数:19
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共 32 条
  • [1] Bandopadhyay T., 2022, ASME Open J. Eng, V1, P011012, DOI [10.1115/1.4053962, DOI 10.1115/1.4053962]
  • [2] A Comprehensive Analytical Shock Loss Model for Axial Compressor Cascades
    Banjac, Milan
    Savanovic, Teodora
    Petkovic, Djordje
    Petrovic, Milan, V
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 144 (09):
  • [3] Understanding of energy conversion and losses in a centrifugal pump impeller
    Chen, Weisheng
    Li, Yaojun
    Liu, Zhuqing
    Hong, Yiping
    [J]. ENERGY, 2023, 263
  • [4] Loss Analysis of Cavity Leakage Flow in a Compressor Cascade
    Deng, Hefang
    Xia, Kailong
    Teng, Jinfang
    Lu, Shaopeng
    Zhu, Mingmin
    Qiang, Xiaoqing
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 144 (12):
  • [5] Denton J.D., 1993, LOSS MECH TURBOMACHI
  • [6] Farokhi S., 2014, AIRCRAFT PROPULSION
  • [7] Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part I-Methodology, Numerical Setup, and Aerodynamic Analysis
    Francois, Benjamin
    Polacsek, Cyril
    Barrier, Raphael
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 144 (11):
  • [8] Goldberg D. E., 1989, GENETIC ALGORITHMS S
  • [9] Spectral proper orthogonal decomposition of compressor tip leakage flow
    He, Xiao
    Fang, Zhou
    Rigas, Georgios
    Vahdati, Mehdi
    [J]. PHYSICS OF FLUIDS, 2021, 33 (10)
  • [10] Effect of the Radial Velocity Distribution on the Loss Generation of a Contra-Rotating Fan in a Ventilation System
    Jia, Xingyu
    Zhang, Xi
    Guo, Kui
    Li, Xuehui
    [J]. ENTROPY, 2023, 25 (03)