• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.403-406
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• 2006

PW206C 터보샤프트엔진을 장착한 스마트무인기의 엔진베이 냉각을 목적으로 하는 이젝터를 설계하였다. 이젝터의 기하학적 형상과 유량비의 관계를 근사적 해석식을 사용하여 계산하므로서 이젝터의 형상을 설계하고 성능을 분석하였다. 근사적 해석식의 결과를 검증하기 위해 Fluent 코드를 이용하여 난류 유동해석을 수향하였다. Fluent 코드로 계산한 유량은 근사적 해석식으로 계산한 결과와는 차이를 보였으며, 이것은 이젝터 내부에서 유동의 충분한 혼합이 이루어지지 못하기 때문이다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1999년도 하계학술대회 논문집 A
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• pp.376-378
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• 1999

In order to design the current carrying conductor for GIS, it is important to predict temperature-rise when rated current flows. This paper deals with the coupling of Flux2D and analytic method to calculate the heat transfer coefficient. Heat transfer by conduction and convection is considered between the current carrying conductor and $SF_6$ gas. The result shows reasonable temperature distribution.

• 한국전산유체공학회지
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• 제7권3호
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• pp.53-59
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• 2002

A two-dimensional laminar flow through a channel with a pair of symmetric vertical fins is investigated. At far up- and down-stream from the fins, the plane Poiseuille flow exists in the channel. The Stokes flow for this channel is first investigated analytically and then the other laminar flows by numerical method. For analytic method, the method of eigen function expansion and collocation method are employed. In numerical solution for laminar flows, finite difference method(FDM) is used to obtain vorticity and stream function. From the results, the streamline patterns are shown and the additional pressure drop due to the attached fins and the force exerted on the fin are calculated. It is clear that the force depends on the length of fins and Reynolds number. When the Reynolds number exceeds a critical value, the flow becomes asymmetric. This critical Reynolds number Re/sub c/ depends on the length of the fins.

• 제어로봇시스템학회논문지
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• 제19권6호
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• pp.563-568
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• 2013

The purpose of this study is to find the analytic solution for determining the optimal capacity (lot-size) of a batch-storage network to meet the finished product demand under infrequent shutdowns. Batch processes are bound to experience random but infrequent operating time losses. Two common remedies for these failures are duplicating another process or increasing the process and storage capacity, both of which are very costly in modern manufacturing systems. An optimization model minimizing the total cost composed of setup and inventory holding costs as well as the capital costs of constructing processes and storage units is pursued with the framework of a batch-storage network of which flows are susceptible to infrequent shutdowns. The superstructure of the plant consists of a network of serially and/or parallel interlinked batch processes and storage units. The processes transform a set of feedstock materials into another set of products with constant conversion factors.A novel production and inventory analysis method, the PSW (Periodic Square Wave) model, is applied. The advantage of the PSW model stems from the fact it provides a set of simple analytic solutions in spite of a realistic description of the material flow between processes and storage units. The resulting simple analytic solution can greatly enhance a proper and quick investment decision at the early plant design stagewhen confronted with diverse economic situations.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 추계학술대회 논문집(제1권)
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• pp.339-344
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• 2006

지속적인 컨테이너 물동량의 증가와 컨테이너선의 대형화에 따라서 항만간의 경쟁은 점점 치열해지고 있다. 주요 항만 하역장비 제작 업체들은 획기적인 생산성 향상을 제공할 수 있는 새로운 개념의 하역장비 개발에 많은 관심을 기울이고 있다. 본 연구에서는 항만의 대표적 하역 장비인 컨테이너 크레인에 대해서 다양한 개발 대안들이 존재할 때, 최적의 개발 대안을 선정하는 2단계 절차를 제시한다. 절차는 두 단계로 구성되는데, 첫 번째 단계에서는 요구되는 필수사항들을 만족하지 못하는 대안을 제거하고 두 번째 단계에서는 AHP(Analytic Hierarchy Process)를 적용하여 최종적인 개발 대안을 선정한다. 마지막으로, 제시한 절차를 적용한 예제를 제시한다.

• 한국전산유체공학회지
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• 제4권1호
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• pp.19-26
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• 1999

This paper describes a numerical method for predicting the incompressible unsteady laminar three-dimensional flows with free-surface. The Navier-Stokes equations governing the flows have been discretized by means of finite-difference approximations, and the resulting equations have been solved via the SIMPLE-C algorithm. The free-surface is defined by the motion of a set of marker particles and the interface behaviour was investigated by means of a "Lagrangian" technique. Using the GALA concept of Spalding, the conventional mass continuity equation is modified to form a volumetric or bulk-continuity equation. The use of this bulk-continuity relation allows the hydrodynamic variables to be computed over the entire flow domain including both liquid and gas regions. Thus, the free-surface boundary conditions are imposed implicitly and the problem formulation is greatly simplified. The numerical procedure is validated by comparing the predicted results of a periodic standing waves problems with analytic solutions. The results show that this numerical method produces accurate and physically realistic predictions of three-dimensional free-surface flows.

• 천문학회보
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• 제36권2호
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• pp.56.2-56.2
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• 2011

Building a relativistic magnetohydrodynamic (RMHD) codes based on upwind schemes is a challenging project, because the characteristic wave structures for RMHDs has not yet been analytically given. We obtained an analytic expression of eigenvalues and eigenvectors of the flux Jacobian matrix of RMHDs for one-dimensional, isothermal flows with two velocity and magnetic field components (that is, x and y components only), which can be used to build numerical codes. The degeneracies were taken into account. Here, we present preliminary test results with an RMHD code based on the total variation diminishing (TVD) scheme.

• 한국항공우주학회지
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• 제30권7호
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• pp.90-97
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• 2002

희박 상태 비행체 외부 및 추진장치 내부 유동이나 MEMS 장치의 기체유동은 높은 열적 비평형성으로 인해 벽면 슬립모델을 필요로 한다. 조절계수와 벽면속도 구배를 바탕으로 하는 Maxwell 조건이 주로 사용되어 왔지만, 조절계수를 자체적으로 정의할 수 없고, 일차 미분 형태로 인해 실제 적용시 수치적 관점에서 효율적이지 못한 어려움이 있었다. 본 연구에서는 이 문제를 해결하고자 Langmuir의 벽면-기체입자 흡착이론을 이용한다. 벽면온도, 벽면-기체입자간 물리적 힘의 함수인 조절계수를 유도하고, 입자형태의 차이를 감안할 수 있는 물리적 슬립모델을 개발하여 기존 Maxwell 모델과 비교하였다. 또한 내부, 외부, 열유체 유동에 관한 슬립모델의 해석적 해를 실험값과 비교하여 그 유용성을 확인하였다.

• 대한조선학회논문집
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• 제50권6호
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• pp.436-449
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• 2013

In this paper, a numerical analysis is carried out to study the characteristics of supercavitating flows and the drag of relatively simple two-dimensional and axisymmetric bodies which can be used for supercavity generation device, cavitator, of a high-speed underwater vehicle. In order to investigate the suitability of numerical models, cavity flows around the hemispherical head form and two-dimensional wedge are calculated with combinations of three turbulence models(standard $k-{\epsilon}$, realizable $k-{\epsilon}$, Reynolds stress) and two cavitation models(Schnerr-Sauer, Zwart-Gerber-Belamri). From the results, it is confirmed that the calculated cavity flow is more affected by the turbulence model than the cavitation model. For the calculation of steady state cavity flows, the convergence in case of the realizable $k-{\epsilon}$ model is better than the other turbulence models. The numerical result of the Schnerr-Sauer cavitation model is changed less by turbulence model and more robust than the Zwart-Gerber-Belamri model. Thus the realizable $k-{\epsilon}$ turbulence model and the Schnerr-Sauer cavitation model are applied to calculate supercavitating flows around disks, two dimensional $10^{\circ}$ and $30^{\circ}$ wedges. In case of the disk, the cavitation number dependences of the cavity size and the drag coefficient predicted are similar to either experimental data or Reichardt's semi-empirical equations, but the drag coefficient is overestimated about 3% higher than the Reichardt's equation. In case of the wedges, the cavitation number dependences of the cavity size are similar to experimental data and Newman's linear theory, and the agreement of the cavity length predicted and Newman's linear theory becomes better as decreasing cavitation number. However, the drag coefficients of wedges agree more with experimental data than those of Newman's analytic solution. The cavitation number dependences of the drag coefficients of both the disk and the wedge appear linear and simple formula for estimating the drag of supercavitating disks and wedges are suggested. Consequently, the CFD scheme of this study can be applied for numerical analysis of supercavitating flows of the cavitator and the cavitator design.

• Ocean Systems Engineering
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• 제1권1호
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• pp.31-57
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• 2011

Impact pressure due to sloshing is of great concern for the ship owners, designers and builders of the LNG carriers regarding the safety of LNG containment system and hull structure. Sloshing of LNG in partially filled tank has been an active area of research with numerous experimental and numerical investigations over the past decade. In order to accurately predict the sloshing impact load, a new numerical method was developed for accurate resolution of violent sloshing flow inside a three-dimensional LNG tank including wave breaking, jet formation, gas entrapping and liquid-gas interaction. The sloshing flow inside a membrane-type LNG tank is simulated numerically using the Finite-Analytic Navier-Stokes (FANS) method. The governing equations for two-phase air and water flows are formulated in curvilinear coordinate system and discretized using the finite-analytic method on a non-staggered grid. Simulations were performed for LNG tank in transverse and longitudinal motions including horizontal, vertical, and rotational motions. The predicted impact pressures were compared with the corresponding experimental data. The validation results clearly illustrate the capability of the present two-phase FANS method for accurate prediction of impact pressure in sloshing LNG tank including violent free surface motion, three-dimensional instability and air trapping effects.