Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters

Shui Ting Ding; Dong Zhang; Zhi Tao; Guo Qiang Xu

Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters

Shui Ting Ding^*
, Dong Zhang
, Zhi Tao
, Guo Qiang Xu

^*Corresponding author for this work

Research institute of Aero-Engine

Beihang University

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

Numerical simulation was extended with the proposed mixing length equation for the cavity model with realistic engine parameters and the prediction was quite reasonable. It was believed that, for highly non-linear phenomena such as coolant through rotating cavity, this extension was more accurate than direct application of correlations from model tests.

Original language	English
Pages (from-to)	118-121
Number of pages	4
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	24
Issue number	2
State	Published - Apr 2003

Keywords

Aircraft engine
Heat transfer
Mixing length flow theory
Numerical simulation
Turbine wheel

Cite this

@article{5abb41f21d1149a0aadf392c38a8ef84,

title = "Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters",

abstract = "Numerical simulation was extended with the proposed mixing length equation for the cavity model with realistic engine parameters and the prediction was quite reasonable. It was believed that, for highly non-linear phenomena such as coolant through rotating cavity, this extension was more accurate than direct application of correlations from model tests.",

keywords = "Aircraft engine, Heat transfer, Mixing length flow theory, Numerical simulation, Turbine wheel",

author = "Ding, \{Shui Ting\} and Dong Zhang and Zhi Tao and Xu, \{Guo Qiang\}",

year = "2003",

month = apr,

language = "英语",

volume = "24",

pages = "118--121",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "2",

}

TY - JOUR

T1 - Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters

AU - Ding, Shui Ting

AU - Zhang, Dong

AU - Tao, Zhi

AU - Xu, Guo Qiang

PY - 2003/4

Y1 - 2003/4

N2 - Numerical simulation was extended with the proposed mixing length equation for the cavity model with realistic engine parameters and the prediction was quite reasonable. It was believed that, for highly non-linear phenomena such as coolant through rotating cavity, this extension was more accurate than direct application of correlations from model tests.

AB - Numerical simulation was extended with the proposed mixing length equation for the cavity model with realistic engine parameters and the prediction was quite reasonable. It was believed that, for highly non-linear phenomena such as coolant through rotating cavity, this extension was more accurate than direct application of correlations from model tests.

KW - Aircraft engine

KW - Heat transfer

KW - Mixing length flow theory

KW - Numerical simulation

KW - Turbine wheel

UR - https://www.scopus.com/pages/publications/0042027944

M3 - 文章

AN - SCOPUS:0042027944

SN - 1001-4055

VL - 24

SP - 118

EP - 121

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 2

ER -

Numerical simulation for flow and heat transfer of a rotating turbine cavity with realistic engine parameters

Abstract

Keywords

Other files and links

Fingerprint

Cite this