• 한국전산유체공학회지
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• 제5권1호
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• pp.22-26
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• 2000

The flow around a ship is complex, especially, at the stern region of a full ship, where highly curved streamlines, hook-shaped iso-velocity contours, and strong secondary flow exist. To resolve this complex flow, an Algebraic Stress Model(ASM) is applied. The calculations are performed for the HSVA Tanker. The results are improved comparing with those of standard k-ε turbulence model, but still show a little difference from the experiments.

• 한국해양공학회지
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• 제13권2호통권32호
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• pp.138-146
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• 1999

The viscous flow around a ship hull is calculated by the use of RANS(Reynolds-averaged Navier-Stokes) solver. Reynolds stresses are midelled by using the k-${epsilon}$ turbulence model and the law is applied near the body. Body fitted corrdinates are introduced for the treatment of the complex boundary of the ship hull form and the governing equations in the physical domain transformed into ones in the computational domain. The transformed equations are numerically solved by an employment of FVM(Finite Volume Method). SIMPLE(Semi-Implicit Pressure Linked Equation) method is adopted in the calculation of pressure and the solution of the sidcretized equation is obtained by the line-by-line method with the use of TDMA(Tri-Diagonal Matrix Algorithme). To assure the proprietty of this computing method, HSVA tanker and Dyne hull are calculated ar both model and ship scale Reynolds number. Their reaults of pressure distributions on fore and aft body, axial velocity contours and transverse velocity velocity vectors and viscous resistance coefficients are compared with other's experiments and calculations.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1995년도 추계 학술대회논문집
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• pp.118-125
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• 1995

This paper presents the result of a computational study on the wake characteristics of two tanker models. i.e HSVA and DYNE hull forms. The focus of the study is on the distributions of axial. radial and tangential velocities of the two hull forms in way of the propeller, especially over the propeller disk. The effect of bilge vortices on the velocity distribution is also concerned. For the computation of stern and wake flows of the two hull forms. the incompressible Reynolds-Averaged Navier-Stokes(RANS) equations are numerically solved by the use of a second order finite difference method, which employs a four stage Runge-Kutta scheme with a residual averaging technique and the Baldwin-Lomax model. The calculated pressure distributions on the hull surface and the axial. radial and tangential velocity distributions over the propeller disk are presented for the two hull forms. Finally, the result of wake analysis for the computed wake distribution over the propeller disk is given in comparison with those for the experimental wake distribution for the both hull forms.

• 대한조선학회지
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• 제18권2호
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• pp.7-20
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• 1981

A method to predict the three-dimensional turbulent boundary layer on ship forms is introduced. The present differential method is in the scope of thin boundary layer theory and adopting the eddy-viscosity turbulence model. Two different numerical schemes are taken in this paper to handle the sign-changing cross-flows. The method is applied to predict the boundary layer development on real ship forms; SSPA Model 720($C_B$=0.675) and HSVA Tanker Model($C_B$=0.85). The results are qualitatively in good agreements with measurements except at the very stern. Therefore the method seems to be very promising if further developments are accomplished to handle the thick stern boundary layer effectively.

• Journal of Hydrospace Technology
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• 제2권2호
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• pp.1-13
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• 1996

This paper presents the result of a computational study on the wake characteristics of two tanker models, i.e. HSVA and Mystery hull forms. The focus of the study is on the distributions of axial, radial and tangential velocities of the two hull forms in way of the propeller, especially over the propeller disk. The effect of bilge vortices on the velocity distribution is also concerned. For the computation of stern and wake flows of the two hull farms, the incompressible Reynolds-Averaged Wavier-Stokes(RANS) equations are numerically solved by the second order finite difference method, which employs a four stage Runge-Kutta scheme with a residual averaging technique and the Baldwin-Lomax model. The calculated pressure distributions on the hull surface and the axial, radial and tangential velocity distributions over the propeller disk are presented for the two hull forms. Finally, the result of wake analysis for the computed wake distribution over the propeller disk is given in comparison with those for the experimental wake distribution fur the both hull forms.

• 대한조선학회지
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• 제25권4호
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• pp.13-27
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• 1988

TUMMAC차분법(差分法)이 두 가지의 삼차원파(三次元波), 즉 배의 항주(航走)에 따른 파형(波形)과 수직사각주(垂直四角柱) 주위의 쇄파해석(碎波解析)에 적용(適用)되어졌다. Series 60($C_B=0.6$) 모형선(模型船)과 HSVA 모형선(模型船)의 선수부(船首部)에 의한 파형(波形)이 자유표면(自由表面)과 선체후반부(船體後半部)에서의 boundary cell 처리를 엄밀화한 $TUMMAC-IV_{vm1}$방법(方法)에 의하여 계산(計算)되어졌으며, 그 결과가 실제(實際)의 실험결과(實驗結果)들과 비교(比較)되었다. 실험결과(實驗結果)와의 비교를 통하여, $TUMMAC-IV_{vm1}$방법(方法)은 배에 의한 비선형파(非線形波)의 특성해석(特性解析)에 매우 응용성(應用性)이 높음을 보였다. 특히, 비대선형(肥大船型)인 HSVA 모형선(模型船)의 경우는 계산(計算)된 비선형선수파(非線形船首波)의 특성(特性)이 실험결과(實驗結果)와 좋은 일치를 보였다. 수직사각주(垂直四角柱)주위의 쇄파(碎波)를 포함한 심한 비선형파(非線形波)가 삼차원비선형파(三次元非線形波)의 대표적(對表的)인 예(例)로써 TUMMAC-VI 방법(方法)에 의하여 계산(計算)되었다. TUMMAC-VI 방법(方法)은 이층류(二層流)를 함께 푸는 방법(方法)으로, 두가지 유체(流體) 사이의 밀도변화(密度變化), 즉 marker-density를 이용하여 interface를 결정하게 된다. 그러나, 비압축성유체(非壓縮性流體)에 관한 N-S 방정식(方程式)의 해(解)이므로, 그 밖의 계산(計算)에서는 각각의 대표적(對表的)인 밀도(密度)를 사용한다. 계산결과(計算結果)는 삭가주(四角柱) 앞부분의 원형파(圓形波)와 앞어깨에서의 심한 경사를 가지는 파(波), 뒷부분에서의 복잡(複雜)한 쇄파현상(碎波現像)들이 실제의 파특성(波特性)을 잘 나타내어 주었다. TUMMAC-VI 방법(方法)은 interface의 처리를 포함하여 앞으로도 개선(改善)의 여지가 많으며, 단지 공기(空氣)와 물만이 아닌 일반적(一般的)인 이층류(二層流)의 해석에도 폭 넓게 이용될 수 있으리라 본다.