Numerical calculation of transitional boundary layers

E. Arad; M. Berger; M. Israeli; M. Wolfshtein

doi:10.1002/fld.1650020102

Numerical calculation of transitional boundary layers

E. Arad
, M. Berger
, M. Israeli
, M. Wolfshtein

Technion-Israel Institute of Technology

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

10 Scopus citations

Abstract

A computational procedure for compressible axisymmetric boundary layers, on bodies of revolution, in transition from laminar to turbulent flow, is introduced. The procedure is an extension of a former method, due to Patankar and Spalding. The flow field is computed by solution of four simultaneous equations for the momentum, the thermal energy, the turbulence energy amplitude and the turbulent scale. The results show good agreement with existing theoretical and experimental data.

Original language	English
Pages (from-to)	1-23
Number of pages	23
Journal	International Journal for Numerical Methods in Fluids
Volume	2
Issue number	1
DOIs	https://doi.org/10.1002/fld.1650020102
State	Published - 1982
Externally published	Yes

Keywords

Boundary Layers
Models of Turbulence
Transition

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10.1002/fld.1650020102

Cite this

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title = "Numerical calculation of transitional boundary layers",

abstract = "A computational procedure for compressible axisymmetric boundary layers, on bodies of revolution, in transition from laminar to turbulent flow, is introduced. The procedure is an extension of a former method, due to Patankar and Spalding. The flow field is computed by solution of four simultaneous equations for the momentum, the thermal energy, the turbulence energy amplitude and the turbulent scale. The results show good agreement with existing theoretical and experimental data.",

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author = "E. Arad and M. Berger and M. Israeli and M. Wolfshtein",

year = "1982",

doi = "10.1002/fld.1650020102",

language = "אנגלית",

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AU - Arad, E.

AU - Berger, M.

AU - Israeli, M.

AU - Wolfshtein, M.

PY - 1982

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AB - A computational procedure for compressible axisymmetric boundary layers, on bodies of revolution, in transition from laminar to turbulent flow, is introduced. The procedure is an extension of a former method, due to Patankar and Spalding. The flow field is computed by solution of four simultaneous equations for the momentum, the thermal energy, the turbulence energy amplitude and the turbulent scale. The results show good agreement with existing theoretical and experimental data.

KW - Boundary Layers

KW - Models of Turbulence

KW - Transition

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DO - 10.1002/fld.1650020102

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JO - International Journal for Numerical Methods in Fluids

JF - International Journal for Numerical Methods in Fluids

IS - 1

ER -

Numerical calculation of transitional boundary layers

Abstract

Keywords

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