RESEARCH ON THE EFFECT OF BOUNDARY LAYER INGESTION OF BLENDED-WING-BODY AIRCRAFT WITH DISTRIBUTED PROPULSION

被引：0
|
作者：
Qiu, Aoxiang [1 ,2 ]
Sang, Weimin [1 ,2 ]
Zhang, Tong [3 ]
An, Bo [1 ,2 ]
Li, Dong [1 ,2 ]
Zhang, Binqian [1 ,2 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
[2] National Key Laboratory of Aircraft Configuration Design, Xi'an,710072, China
[3] AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., Chengdu,610037, China
来源：
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics | 2024年 / 56卷 / 08期
关键词：
Airships - Ducted fan engines - Ducts - Gas turbines - Navier Stokes equations - Reynolds number - Solvent extraction - Supersonic aircraft - Turbomachine blades;
D O I：
10.6052/0459-1879-23-552
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2448 / 2467
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