• Proceedings of the KAIS Fall Conference
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• 2010.11b
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• pp.546-550
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• 2010

무인잠수정이 원하는 경로를 추종할 수 있도록 안정적인 운항제어를 수행하기 위해서는 잠수정의 동역학적 특성을 정확히 파악하는 것이 필요하다. 수중에서 거동하는 무인잠수정의 동역학적 특성은 제어입력뿐만 아니라 유체력계수에 의해 주로 결정되므로, 이러한 계수값을 정확하게 아는 것이 중요한 요소라 할 수 있다. 일반적으로 유체력계수는 PMM 시험과 같은 실험적 방법을 통하여 얻게 되지만 실험방법의 어려움과 실험장비들의 부정확성으로 인한 오차에 의하여, 얻어진 값들의 신뢰성이 많이 저하된다. 계수값들을 구할 수 있는 다른 방법으로는, 확장칼만필터 등과 같은 모델기반 추정 알고리즘을 통하여 유체력계수를 추정하는 것이다. 본 논문에서는 확장칼만필터를 이용하여 유체력계수를 추정하도록 하였으며, 설계된 추정 알고리즘의 성능을 검증하기 위하여 기존에 수행된 PMM 시험에 의해 얻어진 유체력계수의 실험값과 비교 분석하였다. 또한 본 논문에서는 만타형 무인잠수정을 이용하여 원하는 경로를 추종할 수 있도록, 추정된 유체력계수를 사용하여 수심제어 및 방향제어를 위한 슬라이딩 모드 제어기를 설계하였으며, 충분한 정확도를 가지고 원하는 경로를 추종함을 시뮬레이션을 통해 확인하였다.

• The KSFM Journal of Fluid Machinery
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• v.2 no.3 s.4
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• pp.52-58
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• 1999

The leakage and rotordynamic coefficients of see-through type gas labyrinth seals are determined using a two-control-volume-model analysis with Moody's wall-friction-factor formula which is defined with a large range of Reynolds number and relative roughness. Jet flow theory are used for the calculation of the recirculation velocity in the cavity. For the reaction force from the labyrinth seal, linearized zeroth-order and the first-order perturbation equations are developed for small motion about a centered position. The leakage and rotordynamic coefficient results of the present analysis are compared with Scharrer's theoretical analysis using Blasius' wall-friction-factor formula and Pelletti's experimental results. The comparison shows that the present analysis using Moody's wall-friction-factor formula and Scharrer's theoretical analysis using Blasius' wall-friction-factor formula give the same results for a smooth seal surface and the range of Reynolds number less than $10^5$.

• Journal of the Society of Naval Architects of Korea
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• v.43 no.4 s.148
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• pp.460-466
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• 2006

The three-dimensional RANS equations were applied to analyze the flow field of a submarine. To validate the code, the DARPA SUBOFF bare hull and an eliipsoid at angles of attack of $10^{\circ}\;and\;30^{\circ}$ were simulated and good agreement with experiments was obtained. After the code validation, the flows over the full configuration of DARPA SUBOFF model having a fairwater and four stern appendages were simulated at four angles of attack $(0^{\circ},\;10^{\circ},\;20^{\circ},\;30^{\circ})$ and three yaw angles $(10^{\circ},\;20^{\circ},\;30^{\circ})$ Specifically, the pressure contours and streamlines of fairwater and stern appendage were compared as the angle of attack and yaw angle changed. The variations of hydrodynamic forces were also calculated.

• The KSFM Journal of Fluid Machinery
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• v.4 no.2 s.11
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• pp.15-21
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• 2001

Basic equations and their solution procedure we derived for the analysis of an annular pump seal in which the rotor has a large static displacement from the centered position. The Bulk-flow is assumed for a control volume set in the seal clearance and the flow is assumed to be completely turbulent in axial and circumferential direction. Moody's wall-friction-factor formula is used for the calculation of wall shear stresses in the control volume. For the reaction force developed by the seal, linearized zeroth-order and first-order perturbation equations are developed for small motion about an eccentric position. Flow variables are expanded by using Fourier series for the solution procedure. Integration of the resultant first-order pressure distribution along and around the seal defines the 12 elements of rotordynamic coefficients of the eccentric annular pump seal. The results of leakage and rotordynamic coefficients aye presented and compared with the Marquette's experimental results and the San Andres' theoretical analysis.

• Journal of the Korean Society of Marine Environment & Safety
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• v.25 no.5
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• pp.627-633
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• 2019

This study aimed to predict the resistance and propulsion performance of a ship using computational fluid dynamics (CFD) and a database as well as establish an assessment method for the energy efficiency design index (EEDI) using the results. First, the total resistance of the studied ship is obtained using CFD. A flow analysis is conducted with the free surface and trim and sinkage using a commercial CFD code (STAR-CCM+). The effective power of the ship is assessed based on the CFD results. The quasi-propulsive efficiency is calculated from an empirical prediction equation using experimental data and similar material. Finally, a general calculation program for the EEDI is established based on the hydrodynamic results, ship information for principal particulars, conversion factor of $CO_2$ for fuels, and fuel consumption.

• Journal of the Society of Naval Architects of Korea
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• v.49 no.4
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• pp.287-295
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• 2012

Hydrodynamic performance of a movable submerged breakwater was analyzed using energy dissipation model. Based on two-dimensional boundary element method the equation of motion including a viscous dissipation term proportional to velocity squared was solved by Newton-Raphson method. Energy dissipation coefficients as well as reflection and transmission coefficients of a submerged flat plate were calculated with various plate lengths and thickness. Both real and imaginary components of body displacement and forces were used to solve the motion of breakwater accurately. The effect of the magnitude of dissipation coefficient on the body displacement was evaluated. The results from the potential theory with no dissipation term were found to be an overestimate in resonance frequency.

• The KSFM Journal of Fluid Machinery
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• v.4 no.3 s.12
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• pp.29-38
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• 2001

The floating ring seal has the ability of minimizing clearance without the rubbing phenomenon. It is often used in the turbo pump units of liquid rocket engines due to its superior leakage performance. The exact prediction of the lock-up position of the floating ring, the leakage performance, and the rotordynamic coefficients of the seal is necessary to evaluate the rotordynamic performance of the turbo pump unit. The governing equations(which are based on the Bulk-flow Model) we solved by the Fast Fourier Transform method. The lock-up position, leakage flow rate, and rotordynamic coefficients are evaluated according to the geometric parameters of the floating ring seal.

• The KSFM Journal of Fluid Machinery
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• v.18 no.1
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• pp.44-50
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• 2015

Labyrinth seals are commonly used in various kinds of turbomachinery to reduce leakage flow. In the present 3D CFD analysis of see-through-type labyrinth air seal, the methodology of determining leakage and rotordynamic coefficients is suggested with the relative coordinate system for steady-state simulation. The leakage flow and rotordynamic forces predicted by using different solvers and turbulent models of FLUENT are compared with the results of the existing bulk-flow analysis code LABYSEAL.FOR and experiment. The present CFD result of direct stiffness(K) shows only improvement in prediction. The results of leakage and rotordynamic coefficients as well as computing time are sensitive against the used solver and turbulent model.

• Proceedings of the Korea Water Resources Association Conference
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• 2012.05a
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• pp.587-587
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• 2012

현재 대부분 하천관리의 흐름해석에서 주가 되었던 1차원 분석은 하천 단면에 따른 횡적인 수면차, 유속분포를 분석할 수 없다는 단점을 가지고 있으며, 특히 유량 및 유속이 급속도로 늘어나는 홍수시에는 그 오차가 더욱 커질 수 있다. 반면에 2차원 모형의 흐름해석은 사행하천의 흐름 특성과 만곡부에서의 종 횡방향 수면경사 및 양안의 수면차와 합류지점의 횡방향 흐름 등의 영향을 고려할 수 있으며 1차원 해석과는 달리 전 단면에 걸쳐 유속 및 수위 분포를 나타낼 수 있어 실제흐름에 가까운 수리량을 얻을 수 있다. 본 연구를 위해 적용된 해석모형인 SMS는 미국 Brigham Young 대학의 환경모형연구실과 미공병단(USACE)의 수로실험국(WES) 등에서 개발한 프로그램으로서 RMA2, RMA4, SED2D 모형 등으로 구성되어 있다. 각각의 모형은 수리 동역학적 해석, 오염물 이송확산 해석, 유사의 이송 및 퇴적 해석이 가능하며 이 중 RMA2를 이용한 2차원 흐름해석을 통하여 보다 적합한 하천관리에 이용가능하도록 하고자 한다. 연구대상 지역은 제주도 한천 하류부로서 제주도 하천 특성상 평상시 건천의 상태를 이루고 있으나 태풍 및 집중호우시 홍수유출이 발생하여 수위가 급격하게 상승하는 양상을 보인다. 대표적인 예로 태풍 '나리'시 최대 일강우량 420mm로 인한 인근 지역에 0.5 ~ 1.5m의 침수흔적을 보이고 있다. 본 연구에서는 2011년 최고수위를 기록한 태풍 '무이파'를 대상으로 하였으며 대상지역의 Kalesto를 이용한 수위-유속 자료를 이용하여 산출된 유량을 경계조건으로 사용하였고 격자망 형성을 위한 지형 데이터는 지형도 및 측량자료를 이용하여 구축하였다. 사용된 대표적인 매개변수는 하상의 조도계수를 나타내는 Manning의 n값과 유체의 밀도, 속도구배, 구조 등 여러 가지의 유체조건에 따라 변하는 성질인 와점성계수(eddy viscosity)로 요약할 수 있으며 Manning의 n값은 하천설계기준에 따른 하천기본계획의 조도계수를 사용하였고 와점성계수는 적합한 흐름 분포를 결정하기 위해 흐름이 안정될 때까지 변화시켜 해석을 시행하였다. 해석결과 만곡부에서는 급한 흐름을 보이고 있으며 최대하폭 구간에서는 완만한 흐름이 나타나 사행하천의 흐름특성과 횡적인 하천단면에 따른 변화, 하상고 차이로 인한 유속분포를 확인할 수 있으며 이는 보다 유용한 하천관리에 이용가능할 것으로 사료된다.

• The KSFM Journal of Fluid Machinery
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• v.7 no.6 s.27
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• pp.21-27
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• 2004

The floating ring seal has an advantage to find the optimum position by itself, which is used in the turbo pump of a liquid rocket. The main purpose of seals is to reduce the leakage. Especially, seals of the turbo pump for the liquid rocket engine are operated under the serious conditions such as high pressure above 10 MPa, very low temperature about $-180^{\circ}C$ and high rotating speed above 25,000 rpm. So, rotordynamic stability is very important for the system stability. In this paper, the leakage and dynamic characteristics of floating ring seals were investigated by a experimental and analytical method. The theoretical results of the leakage performance for the floating ring seal showed much higher than that of experimental results. On the other hand, the results of stiffness and damping characteristics showed similarity each other. As the shaft speed was increasing, the whirl frequency ratio was increased in the experimental results.