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선박의 저항성능 추정을 위한 EARSM 난류 모형의 활용Numerical prediction of ship hydrodynamic performances using explicit algebraic Reynolds stress turbulence model

Other Titles
Numerical prediction of ship hydrodynamic performances using explicit algebraic Reynolds stress turbulence model
Authors
김유철김광수김진
Issue Date
19-2월-2014
Publisher
대한조선학회
Keywords
EARSM; Turbulence model; Reynolds stress; Wake distribution
Citation
대한조선학회논문집, v.51, no.1, pp 67 - 77
Pages
11
Journal Title
대한조선학회논문집
Volume
51
Number
1
Start Page
67
End Page
77
URI
https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/8133
Abstract
In this study, Explicit Algebraic Reynolds Stress Model (EARSM) which is based on the existing k-epsilon model has been applied to the flow field analysis around ship hulls. Existing transport equations for the turbulent kinetic energy and the dissipation rate are used in almost the same form and anisotropy terms of Reynolds stresses are newly considered. The well-known KVLCC2 and KCS hull forms are selected as validation cases, which were also used in 2010 Workshop on CFD in Ship Hydrodynamics. In case of KVLCC2 double model, comparison of mean velocity distribution, turbulent kinetic energy, and Reynolds stresses near the propeller plane has been carried out and wave elevation and wave profiles have been additionally studied for KCS and KVLCC2 with free surface models. Some improved results for mean velocity distribution at the propeller plane have been obtained while there is little change in free surface wave profiles.the dissipation rate are used in almost the same form and anisotropy terms of Reynolds stresses are newly considered. The well-known KVLCC2 and KCS hull forms are selected as validation cases, which were also used in 2010 Workshop on CFD in Ship Hydrodynamics. In case of KVLCC2 double model, comparison of mean velocity distribution, turbulent kinetic energy, and Reynolds stresses near the propeller plane has been carried out and wave elevation and wave profiles have been additionally studied for KCS and KVLCC2 with free surface models. Some improved results for mean velocity distribution at the propeller plane have been obtained while there is little change in free surface wave profiles.
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