空气动力学学报2016,Vol.34Issue(2):267-275,9.DOI:10.7638/kqdlxxb-2016.0002
HyperFLOW亚跨声速流动验证
Validation of HyperFLOW in Subsonic and Transonic Flow
摘要
关键词
HyperFLOW/CFD软件/NASA Trap-Wing高升力外形/DLR-F6翼身组合体Key words
HyperFLOW/CFD Software/NASA Trap-Wing high-lift model/DLR-F6 wing-body分类
航空航天引用本文复制引用
赫新,赵钟,马戎,王年华,张来平..HyperFLOW亚跨声速流动验证[J].空气动力学学报,2016,34(2):267-275,9.基金项目
Supported by National Science Foundation of China (No.11272339) (No.11272339)