Simulation of boundary layer transition

Lin Yang; Zheng Ping Zou; Fang Fei Ning; Mao Zhang Chen

Simulation of boundary layer transition

Lin Yang^*
, Zheng Ping Zou
, Fang Fei Ning
, Mao Zhang Chen

^*此作品的通讯作者

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

16 引用（Scopus）

摘要

The Abu-Ghannam and Shaw (AGS) model was added to the turbulent model in order to simulate the process of laminar to turbulent transition. Flat plate and turbine cascade boundary layer was studied and compared to the experimental data. The results show that the transition process could be better simulated by the transition model, but the simulation shows little deviation from the test data under great change of pressure gradient.

源语言	英语
页（从-至）	355-360
页数	6
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	20
期	3
出版状态	已出版 - 6月 2005

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链接到 Scopus 的出版物

引用此

@article{f4200bd2c16f4f458f69a104aa032458,

title = "Simulation of boundary layer transition",

abstract = "The Abu-Ghannam and Shaw (AGS) model was added to the turbulent model in order to simulate the process of laminar to turbulent transition. Flat plate and turbine cascade boundary layer was studied and compared to the experimental data. The results show that the transition process could be better simulated by the transition model, but the simulation shows little deviation from the test data under great change of pressure gradient.",

keywords = "Aerospace propulsion system, Boundary layer transition, Flat plate, Simulation, Turbine",

author = "Lin Yang and Zou, \{Zheng Ping\} and Ning, \{Fang Fei\} and Chen, \{Mao Zhang\}",

year = "2005",

month = jun,

language = "英语",

volume = "20",

pages = "355--360",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

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number = "3",

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TY - JOUR

T1 - Simulation of boundary layer transition

AU - Yang, Lin

AU - Zou, Zheng Ping

AU - Ning, Fang Fei

AU - Chen, Mao Zhang

PY - 2005/6

Y1 - 2005/6

N2 - The Abu-Ghannam and Shaw (AGS) model was added to the turbulent model in order to simulate the process of laminar to turbulent transition. Flat plate and turbine cascade boundary layer was studied and compared to the experimental data. The results show that the transition process could be better simulated by the transition model, but the simulation shows little deviation from the test data under great change of pressure gradient.

AB - The Abu-Ghannam and Shaw (AGS) model was added to the turbulent model in order to simulate the process of laminar to turbulent transition. Flat plate and turbine cascade boundary layer was studied and compared to the experimental data. The results show that the transition process could be better simulated by the transition model, but the simulation shows little deviation from the test data under great change of pressure gradient.

KW - Aerospace propulsion system

KW - Boundary layer transition

KW - Flat plate

KW - Simulation

KW - Turbine

UR - https://www.scopus.com/pages/publications/22844440441

M3 - 文章

AN - SCOPUS:22844440441

SN - 1000-8055

VL - 20

SP - 355

EP - 360

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 3

ER -

Simulation of boundary layer transition

摘要

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