Numerical Analysis of the Thermal–Hydraulic Performance of Supercritical Liquefied Natural Gas in Airfoil Fin PCHEs

Author:

Meng Xiangfeng12,Yuan Qiuyang3,Li Yaning3,Lin Xiaochen3,Liu Na3

Affiliation:

1. Qingdao University of Technology School of Environmental and Municipal Engineering, , 777 Jialingjiang Road, Huangdao District, Qingdao 266520 , China ;

2. Sinopec Petroleum Engineering Corporation , Dongying 257026 , China

3. Qingdao University of Technology School of Environmental and Municipal Engineering, , 777 Jialingjiang Road, Huangdao District, Qingdao 266520 , China

Abstract

Abstract As a novel, compact, and efficient plate-fin heat exchanger, the Printed Circuit Heat Exchanger (PCHE) is a prospective candidate for liquefied natural gas (LNG) vaporization at low-temperature and high pressure. Generally, the airfoil fin PCHE has better thermal–hydraulic performance than the zigzag channel PCHE. In this study, the thermal–hydraulic performance of supercritical LNG in PCHEs with different airfoil fin types and arrangements is investigated by numerical simulations. First, the effects of six different airfoil fin types, NACA0010, NACA0020, NACA0025, NACA0030, NACA 0040, and NACA 0050, on the thermal–hydraulic performances were studied. The results show that NACA0025 has the best comprehensive heat transfer performance. Then, the effects of the airfoil fin arrangement's staggered, vertical, and horizontal pitch on thermal–hydraulic performance were investigated. The results show that the optimal values of the dimensionless number for staggered and vertical arrangements are 1 and 4, respectively. The comprehensive performance does not change much when the dimensionless horizontal pitch number exceeds 3.0. Finally, the thermal–hydraulic performance of uniformly distributed, three front sparse and rear dense, and three front-dense and rear-sparse distributed airfoil fins was investigated. The results show that the front-dense and rear-sparse airfoil fins enhance and the front-sparse and rear-dense airfoil fins reduce the comprehensive performance compared to the uniform arrangement. The results show that a denser arrangement of airfoil fins near the quasi-critical point can improve the comprehensive performance while keeping the number of airfoil fins constant.

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shandong Province

Publisher

ASME International

Subject

Fluid Flow and Transfer Processes,General Engineering,Condensed Matter Physics,General Materials Science

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3