Extensions of menter's SST transition model to simulate hypersonic and crossflow transition

Zhang Xiaodong; Gao Zhenghong; Zhong Bowen

Extensions of menter's SST transition model to simulate hypersonic and crossflow transition

Zhang Xiaodong, Gao Zhenghong, Zhong Bowen

School of Aeronautics

Research output: Contribution to conference › Paper › peer-review

3 Scopus citations

Abstract

An improvement based on menter's transition model has been made to expand its application in this paper. A compressibility correlation is added into the original model to simulate the hypersonic flow transition problem. The double wedge flat plate is numerically tested to validate the modified model, the computational results shows good agreement compared with the experiment data. Furthermore, a preliminary investigation of cross-flow instability on the NLF 0415 swept wing is made in the last section of this paper.

Original language	English
Pages	1603-1611
Number of pages	9
State	Published - 2012
Event	28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012 - Brisbane, Australia Duration: 23 Sep 2012 → 28 Sep 2012

Conference

Conference	28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012
Country/Territory	Australia
City	Brisbane
Period	23/09/12 → 28/09/12

Keywords

Boundary layer
Compressibility correlation
Hypersonic
Transition model

Cite this

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title = "Extensions of menter's SST transition model to simulate hypersonic and crossflow transition",

abstract = "An improvement based on menter's transition model has been made to expand its application in this paper. A compressibility correlation is added into the original model to simulate the hypersonic flow transition problem. The double wedge flat plate is numerically tested to validate the modified model, the computational results shows good agreement compared with the experiment data. Furthermore, a preliminary investigation of cross-flow instability on the NLF 0415 swept wing is made in the last section of this paper.",

keywords = "Boundary layer, Compressibility correlation, Hypersonic, Transition model",

author = "Zhang Xiaodong and Gao Zhenghong and Zhong Bowen",

year = "2012",

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note = "28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012 ; Conference date: 23-09-2012 Through 28-09-2012",

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AU - Xiaodong, Zhang

AU - Zhenghong, Gao

AU - Bowen, Zhong

PY - 2012

Y1 - 2012

N2 - An improvement based on menter's transition model has been made to expand its application in this paper. A compressibility correlation is added into the original model to simulate the hypersonic flow transition problem. The double wedge flat plate is numerically tested to validate the modified model, the computational results shows good agreement compared with the experiment data. Furthermore, a preliminary investigation of cross-flow instability on the NLF 0415 swept wing is made in the last section of this paper.

AB - An improvement based on menter's transition model has been made to expand its application in this paper. A compressibility correlation is added into the original model to simulate the hypersonic flow transition problem. The double wedge flat plate is numerically tested to validate the modified model, the computational results shows good agreement compared with the experiment data. Furthermore, a preliminary investigation of cross-flow instability on the NLF 0415 swept wing is made in the last section of this paper.

KW - Boundary layer

KW - Compressibility correlation

KW - Hypersonic

KW - Transition model

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M3 - 论文

AN - SCOPUS:84896920151

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EP - 1611

T2 - 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012

Y2 - 23 September 2012 through 28 September 2012

ER -

Extensions of menter's SST transition model to simulate hypersonic and crossflow transition

Abstract

Conference

Keywords

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