Hybrid optimization of curvature continuous stacking line on the highly loaded diffuser cascade
Author:
Funder
National Science and Technology Major Project
Fundamental Research Funds for the Central Universities
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42401-023-00265-y.pdf
Reference26 articles.
1. Epstein AH (2014) Aeropropulsion for commercial aviation in the twenty-first century and research directions needed. AIAA J 52(5):901–911
2. Wang YY et al (2002) Influence of stacking line of curved blade on aerodynamic performance of compressor cascade. J Aerosp Power 17(3):327–331
3. Wennerstrom AJ (1990) Highly loaded axial flow compressors: history and current developments. J Turbomach 112(4):567–578
4. Adjei RA, Fan C, Wang WZ et al (2021) Multidisciplinary design optimization for performance improvement of an axial flow fan using free-form deformation. J Turbomach 143(1):011003
5. Xu P, Yu X, Liu B (2014) The effects of blade 3d designs in different orthogonal coordinates on the performance of compressor cascades. Int J Turbo Jet-Engines 31(4):329–345
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