Numerical investigation on the effects of boundary layer ingestion on aerodynamic performance of distributed propulsion system

被引：0
|
作者：
Cui, Rong [1 ,2 ]
Pan, Tianyu [1 ,2 ]
Li, Qiushi [1 ,2 ]
Zhang, Jian [3 ]
机构：
[1] National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing,100191, China
[2] Collaborative Innovation Center for Advanced Aero-Engine, Beijing,100191, China
[3] Department of Major Specific Project, Aero Engine Corporation of China, Beijing,100097, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2018年 / 33卷 / 05期
关键词：
Compilation and indexing terms; Copyright 2024 Elsevier Inc;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Mass transfer - Angle of attack indicators - Lift drag ratio - Supersonic aircraft - Drag - Lift - Boundary layers - Propulsion - Angle of attack - Blending - Shock waves - Wings
引用
收藏
页码：1076 / 1083
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