• 대한조선학회논문집
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• 제39권2호
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• pp.34-44
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• 2002

선체 외판 중 약 70% 정도가 3차원 곡면 형상으로 구성되어 있다. 이러한 3차원 형상을 자동으로 성형하기 위해서 수년간 많은 연구를 수행하여 오고 있는 실정이다. 본 연구의 목적은 가열현상을 합리적으로 대변할 수 있는 역학적 모델을 도입하여 가열 Simulator를 개발하는데 있다. 이를 위해 가열 결과에 영향을 줄 수 있는 가열 위치 ,강판의 두께, 가열 속도 등 다양한 인자로써 실험을 수행하였다. 본 연구에서 개발한 가열 Simulator의 정당성을 입증하고자 몇 가지 모델에 대해 적용하여, 실험결과와 Simulator의 추정치를 비교한 결과 만족할 만한 결과를 나타내었으며, Simulator에 적용된 이론적 배경의 합당성을 확인할 수 있었다.

• 대한조선학회 특별논문집
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• 대한조선학회 2009년도 특별논문집
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• pp.47-51
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• 2009

It is well known that a rudder is influential devices to help ship maintain its stable performances, such as a course-keeping and maneuverability. In the procedures of a commercial ship design proper rudder dimensions (area and shape) ensuring better ship maneuverability have been settled in an initial concept design stage performed by a preceding department, without little structural consideration. It is true that there are time discrepancy between an initial design and a structural analysis stage. Therefore structural analysis results would sometimes cause a rudder to modify its dimensions. Most of these cases, however, ship design and performance tests had been finished. In this matter, only limited modifications of redder could be carried out. Besides, these could also cause bad effects on productivity. Finally, it is necessary to develop a new program considering co-relationship between an initial rudder design and a following work, a structural strength analysis, in order to enhance productivity and minimize a rate of redesign procedures.

• 소성∙가공
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• 제8권1호
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• pp.92-100
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• 1999

A procedure is proposed for determining the initial thickness distribution in oder to produce a specified final thickness distribution for the axisymmetrical superplastic blow forming processes. Weighted parameter is introduced to improve the simple ad $d_traction method and the initial blank thickness distribution is obtained by optimizing the weighted parameter. This method is applied to superplastic free bulging process with the uniform thickness distribution of final shape to confirm its validity. The optimum initial blank thickness distributions is obtained from arbitrary axisymmetrical superplastic blow forming processes such as dome, cone and cylindrical cup forming with die contact. It is concluded that the ad $d_traction method with weighted parameter is an effective method for an optimum blank thickness distribution design.esign.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2005년도 추계학술대회 논문집
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• pp.40-45
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• 2005

Velocity and density distributions of a high-speed and initial $CO_{2}$ jet flow have been analyzed simultaneously by a developed three-dimensional digital speckle tomography and a particle image velocimetry(PIV). Three high-speed cameras have been used for tomography and PIV since a shape of a nozzle for the jet flow is asymmetric and the initial flow is fast and unsteady, The speckle movements between no flow and $CO_{2}$ jet flow have been obtained by a cross-correlation tracking method so that those distances can be transferred to deflection angles of laser rays for density gradients. The three-dimensional density fields for the high-speed $CO_{2}$ jet flow have been reconstructed from the deflection angles by a real-time tomography method and the two-dimensional velocity fields have been calculated by a PIV method simultaneously and instantaneously.

• 한국정밀공학회지
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• 제11권5호
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• pp.134-142
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• 1994

An upper bound elemental technique (UBET) is applied to predict variations of neutral plane and optimal position of the initial billet for rib-wep shaped ring forging. In the analysis, the neutral plane position and velocity fields are determined by minimizing the total power consump- tion with respect to chosen parameters. The degree of die-cavity filling by initial billet-position and the variations of neutral plane by friction condition are investigated. Experiments have been carried out with pure plasticine billets at room temperature. The theoretical predictions of the forging load and the flow pattern are in good agrement with the experimental results.

• 한국자동차공학회논문집
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• 제21권5호
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• pp.97-103
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• 2013

Crash performance of the straight member was studied by FE analysis. One end of model was fixed and the other end was impacted by 1,000kg rigid mass with velocity of 16.0m/sec. The maximum and mean load were discussed to compare crash performance. The members with various section shapes were analyzed and the flange location was changed. Also, spot weld points were added in the initial buckling region to investigate its effect. Final rectangular section model which has flanges at the center and reinforcement in initial buckling region showed high enhancement in crash performance.

• 한국전산구조공학회논문집
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• 제26권1호
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• pp.79-87
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• 2013

레벨셋방법과 헤비사이드 강화를 이용한 아이소-지오메트릭 위상최적설계 방법을 개발하였다. 레벨셋 방법에서는 초기해석영역은 고정되어 있으며 경계는 레벨셋 함수값을 이용한 암시적인 동적 경계로 표현되며, 이는 복잡한 위상적 변화를 용이하게 표현할 수 있게 한다. 헤비사이드 강화는 기존의 기저함수에 내부 경계를 표현하는 강화 함수를 더함으로써 아이소-지오메트릭 해석법의 정밀도를 향상시킨다. 제안된 위상 최적설계 방법은 다음과 같은 이점을 갖는다. 아이소-지오메트릭 해석법을 이용하여 정밀한 기하 형상을 얻을 수 있으며 텐서 곱을 이용하여 정의된 패치의 한계를 헤비사이드 강화를 이용함으로써 해결할 수 있다. 단일 패치를 사용함으로써 연속적인 응력 분포를 얻어낼 수 있을 뿐 아니라 불연속적인 변위장 또한 표현해 낼 수 있다. 레벨셋 방법론이 암시적 동적 경계를 잘 표현하기 때문에 이를 이용하여 헤비사이드 강화를 이용한 아이소-지오메트릭 해석법에서 위상의 변화를 잘 표현해 낼 수 있다.

• International Journal of Aeronautical and Space Sciences
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• 제17권3호
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• pp.423-431
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• 2016

In this study, wing design optimization for long-endurance unmanned aerial vehicles (UAVs) is investigated. The fluid-structure integration (FSI) analysis is carried out to simulate the aeroelastic characteristics of a high-aspect ratio wing for a long-endurance UAV. High-fidelity computational codes, FLUENT and DIAMOND/IPSAP, are employed for the loose coupling FSI optimization. In addition, this optimization procedure is improved by adopting the design of experiment (DOE) and Kriging model. A design optimization tool, PIAnO, integrates with an in-house codes, CAE simulation and an optimization process for generating the wing geometry/computational mesh, transferring information, and finding the optimum solution. The goal of this optimization is to find the best high-aspect ratio wing shape that generates minimum drag at a cruise condition of $C_L=1.0$. The result shows that the optimal wing shape produced 5.95 % less drag compared to the initial wing shape.

• 한국도로학회논문집
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• 제19권4호
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• pp.19-25
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• 2017

PURPOSES : In this paper, the flow of construction material was simulated using computational fluid dynamics in a 2D axisymmetric condition to evaluate the effect of initial or varying material properties on the final shape of a specimen. METHODS : The CFD model was verified by using a well-known analytical solution for a given test condition followed by performing a sensitivity analysis to evaluate the effect of material properties on the final shape of material. Varying dynamic viscosity and yield stress were also considered. RESULTS : The CFD model in a 2D axisymmetric condition agreed with the analytical solution for most yield stress conditions. Minor disagreements observed at high yield stress conditions indicate improper application of the pure shear assumption for the given material behavior. It was also observed that the variation of yield stress and dynamic viscosity during curing had a meaningful effect on the final shape of the specimen. CONCLUSIONS : It is concluded that CFD modeling in a 2D axisymmetric condition is good enough to evaluate fluidal characteristics of material. The model is able to consider varying yield stress and viscosity during curing. The 3D CFD-DEM coupled model may be required to consider the interaction of aggregates in fluid.

• Journal of Mechanical Science and Technology
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• 제18권9호
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• pp.1559-1564
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• 2004

The process design of hot forging, asymmetric to symmetric rib-web shaped steel, which is used for the turnout of express rails has been studied. Owing to the great difference in shape between the initial billet and the final forged product, it is impossible to hot forge the rail in a single stage operation. The numerical simulation for hot forging of asymmetric shape to symmetric shape was carried out by using commercial FEM code, DEFORMTM-2D. For comparison with the simulation results, a experiment of flow analysis using plasticine was also carried out. The results of the flow experiment showed good agreement with those of the simulation.