Rigid-wake analysis of coaxial rotor aerodynamics in forward flight

Ming Chen; Jizhong Hu; Yihua Cao

Rigid-wake analysis of coaxial rotor aerodynamics in forward flight

Ming Chen^*
, Jizhong Hu
, Yihua Cao

^*此作品的通讯作者

航空科学与工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

The rigid-wake mode of coaxial rotor in forward flight was set up based on the analysis of infinite blade rigid-wake mode. The method of aerodynamic characteristics of coaxial rotor in forward flight was studied by rotor geometry, distance between upper and lower rotor and advance ratio. The theoretical results are in good agreement with the experimental data.

源语言	英语
页（从-至）	74-78
页数	5
期刊	Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
卷	30
期	1
出版状态	已出版 - 1月 2004

其它文件与链接

链接到 Scopus 的出版物

引用此

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title = "Rigid-wake analysis of coaxial rotor aerodynamics in forward flight",

abstract = "The rigid-wake mode of coaxial rotor in forward flight was set up based on the analysis of infinite blade rigid-wake mode. The method of aerodynamic characteristics of coaxial rotor in forward flight was studied by rotor geometry, distance between upper and lower rotor and advance ratio. The theoretical results are in good agreement with the experimental data.",

keywords = "Aerodynamic interference, Circulation, Coaxial rotor, Helicopter, Rotary wing aerodynamics",

author = "Ming Chen and Jizhong Hu and Yihua Cao",

year = "2004",

month = jan,

language = "英语",

volume = "30",

pages = "74--78",

journal = "Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics",

issn = "1001-5965",

publisher = "Beijing University of Aeronautics and Astronautics (BUAA)",

number = "1",

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TY - JOUR

T1 - Rigid-wake analysis of coaxial rotor aerodynamics in forward flight

AU - Chen, Ming

AU - Hu, Jizhong

AU - Cao, Yihua

PY - 2004/1

Y1 - 2004/1

N2 - The rigid-wake mode of coaxial rotor in forward flight was set up based on the analysis of infinite blade rigid-wake mode. The method of aerodynamic characteristics of coaxial rotor in forward flight was studied by rotor geometry, distance between upper and lower rotor and advance ratio. The theoretical results are in good agreement with the experimental data.

AB - The rigid-wake mode of coaxial rotor in forward flight was set up based on the analysis of infinite blade rigid-wake mode. The method of aerodynamic characteristics of coaxial rotor in forward flight was studied by rotor geometry, distance between upper and lower rotor and advance ratio. The theoretical results are in good agreement with the experimental data.

KW - Aerodynamic interference

KW - Circulation

KW - Coaxial rotor

KW - Helicopter

KW - Rotary wing aerodynamics

UR - https://www.scopus.com/pages/publications/2542555838

M3 - 文章

AN - SCOPUS:2542555838

SN - 1001-5965

VL - 30

SP - 74

EP - 78

JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

IS - 1

ER -

Rigid-wake analysis of coaxial rotor aerodynamics in forward flight

摘要

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