• Transactions of the Korean Society of Mechanical Engineers B
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• v.33 no.2
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• pp.69-78
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• 2009

Cavitating flow simulation is of practical importance for many hydraulic engineering systems, such as pump, turbine, nozzle, injector, etc. In the present work, a solver for cavitating flow has been developed and applied to simulate the flows past axisymmetric cylinders. Governing equations are the two-phase Navier-Stokes equations, comprised of continuity equation of liquid and vapor phase. The momentum equation is in the mixture phase. The solver employed an implicit, dual time, preconditioned algorithm in curvilinear coordinates. Computations were carried out for three axisymmetric cylinders: hemispherical, ogive, and caliber-0 forebody shape. Then, the present calculations were compared with experiments and other numerical results to validate the present solver. Also, the code has shown its capability to accurately simulate the re-entrant jet phenomena and ventilated cavitation. Hence, it has been found that the present numerical code has successfully accounted for cavitating flows past axisymmetric cylinders.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.10a
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• pp.11-11
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• 1999

Sach의 Boring out 측정방법은 튜브 또는 실린더 등의 축대칭 부품의 3차원 잔류 응력을 측정하는데 적용할 수 있다. 이 방법은 잔류응력이 층제거시 이완된 변형율로부터 결정된다는 원리에 근거하고 있다. 적용시 가정사항으로는 1) 잔류응력 분포가 축대칭이어야 하고 2) 응력 분포가 축방향을 따라 균일해야 한다는 것이다. 그러나 실제부품은 길이가 제한되어 있기 때문에 잔류응력 분포가 균일하다는 가정이 적용될 수 없다. 본 연구에서는 시편의 길이 대 외경 비를 변화시켰을 때 유한요소해석을 이용하여 층제거시 이완된 변형율로부터 계산된 측정값과 유한요소 해석값을 비교하여 이 측정방법의 적용한계와 타당성을 조사하였으며 얻어진 결론은 다음과 같다. Sach의 Boring out 측정방법을 적용하기 위해서는 부품의 외경 대 길이 비가 3이상일 경우 측정값과 해석값은 거의 일치하는 경향을 보이며 비가 증가할수록 측정오차가 줄어들 것으로 판단된다.

• Proceedings of the KWS Conference
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• 2010.05a
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• pp.48-48
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• 2010

소형 공조장치용 냉매 압축기 부품인 기계식 제어 밸브는 에어컨 컴프레서의 핵심부품이고 년간 수백만 개가 국내에 수입된다. 이를 국산화 하기 위하여 진공로 속에서의 브레이징 공정이 수반되는 외국제품의 제조공정을 탈피하여 진공 속에서 DC 프로젝션 용접을 수행하는 기법을 개발하였다. 실린더 형상의 캡과 케이스를 맞대고 그 사이에 박판을 삽입한 상태에서 butt welding 방식으로 진행되는 본 공정에서는, 생산성이 높고 서보가압 장치를 사용하여 soft touch 를 구현하므로 프로젝션이 손상되지 않은 상태에서 통전이 시작되고 2 단 가압 및 프로파일 가압이 가능하므로 링(ring)형상의 너깃이 축대칭으로 안정적으로 형성되기 때문에 실린더 내부의 밀봉성능이 우수함을 확인하였다. 진공로 속에서 본 가압장치를 설치하여 간편한 방법으로 실린더 내부의 진공상태를 유지할 수 있기 때문에 진공로 속에서의 브레이징 공정이 적용되는 외국제품보다 생산성이 월등함을 알 수 있다. 본 연구에서 개발된 링 프로젝션(ring projection) 용접기법은 초소형 및 소형 실린더 형상의 부품 내부를 진공으로 유지해야 하는 산업현장에서 당장 적용될 수 있는 혁신적인 용접공정이라 판단된다.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.34 no.5
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• pp.567-573
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• 2010

In this study, we evaluated the structural integrity and weight of a rocket motor with a torispherical dome by size optimization. Size optimization was achieved by first-order and sub-problem methods, using the Ansys Parametric Design Language (APDL). For rapid design verification, a modified 2D axisymmetric finite-element model was used, and the bolt pre-tension load was expressed as function of the ratio of the cross-sectional area. The thickness of the dome and the cylindrical part of the rocket motor were selected as the design parameters. Our results showed that the weight and structural integrity of the rocket motor at the initial design stage could be determined more rapidly and accurately with the modified 2D axisymmetric finite-element model than with the 3D finite-element model; further, the weight of the rocket motor could be saved to maximum of 17.6% within safety limit.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.31 no.4
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• pp.423-434
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• 1995

It was used boundary element method(BEM) and analysed axisymmetric problem to solve hydraulic cylinder for large vessel acting uniform internal pressure(25N/m super(2)) within elastic limit. This paper was utilized the carbon steel tubes for machine structural purposed model, inner radius was 150mm and outer radius was 250mm, axial length was semi-infinite and the isoparametric element was used. The important results obtained in this study were summarized as follows. Radial, tangential and shearing stress occured the maximum stresses(48, -20 and 34MPa) at the inner radius and the minimum stresses(32, -4 and 18MPa) at the outer radius of the hydraulic cylinder for large vessel. But negative signs have meaning compressive stress and stress diminution ratio was about 0.15MPa/mm. The use of isoparametric element raised accuracy and the increment of input data lessened the error in internal point but computer run-time was increased. The double node was improved the internal solutions to settle discontinuity at corner and the double exponential formula lessened error of stress value at boundary neighborhood. And then coincidence between the analytical and exact results is found to be fairly good, showing that the proposed analytical by BEM is reliable.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.3
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• pp.169-176
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• 2019

In the present study, a CFD/DSMC hybrid method performed by a coupled analysis between the CFD method and the DSMC method was developed to obtain the flow information on the rarefied gas flows effectively. Flow simulations around the high speed vehicles on the transition flow regimes were conducted by using the developed method. The FRESH-FX vehicle made of cone and cylinder shapes was considered for the simulations. The results of the hybrid method were compared with the results of the pure CFD and the pure DSMC method to confirm the reliability and efficiency of the hybrid method. It was found that the gradient and the intensity of the shock waves were weakened due to the relatively low density on the transition flow regime. It was confirmed that the results of the hybrid analysis were different to those of the pure CFD analysis and almost identical to those of the pure DSMC analysis. In addition, the computational time of the hybrid method was reduced than that of the pure DSMC method. As a result, it was obtained that the validity and the efficiency of the CFD/DSMC hybrid method.