• 소성∙가공
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• 제7권4호
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• pp.340-346
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• 1998

A kinematically admissible velocity field is developed for the analysis of twisting of the extruded products with elliptical shapes from round billet. The twisting of extruded product is caused by the lin-early increased rotational velocity from the center on the cross-section of the workpiece at the die exit. In the analysis the rotational velocity in angular direction is assumed by the multiplication of radial distance and angular velocity. The angular velocity is zero at the die entrance. The increase rate of angular velocity is determined by the minimization of plastic work. The results of the analysis show that the angular velocity of the extruded product in creases with the die twisting angle, the aspect ratio of product the friction condition, the reduction of area, and decreases with the die length.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1999년도 춘계학술대회논문집
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• pp.111-114
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• 1999

The twisting and extrusion process of the product with involute helical fin from the round billet is developed by the upper bound analysis. The twisting of extruded product is caused by the twisted die surface connecting the die entrance section and the die exit section linearly. In the analysis, the internal shear surface is defined as the curved twisted plane from the taisting of die surface and the shear work is calculated by the consumption of shear energy The increase rate of angular velocity is determined by the minimization of plastic work. The results of the analysis show that the angular velocity of the extruded product increases with the die twisting angle, the reduction of area, and decreases with the die length, the friction condition.

• 소성∙가공
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• 제8권2호
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• pp.143-151
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• 1999

The twisting and extrusion process of the product with trapezoidal helical fin from the round billet is developed by the upper bound analysis. The twisting of extruded product is caused by the twisted die surface connecting the die entrance section and the die exit section linearly. In the analysis, the rotational velocity in angular direction is assumed by the multiplication of radial distance and angular velocity. The angular velocity is increased linearly by axial distance from the die entrance. The increase rate of angular velocity is determined by the minimization of plastic work. The results of the analysis show that the angular velocity of the extruded product increases with the die twisting angle, the reduction of area, and decreases with the die length, the friction condition.

• 소성∙가공
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• 제9권6호
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• pp.574-581
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• 2000

A vertically-walled auto-body part is one of the most difficult stamping parts because of angle change, wall curl, and twisting of the blank after springback as well as fracture and wrinkle. In this study, computational simulations of the vertically-walled auto-body part are carried out focusing on angle change, wall curl, and twisting after springback. Binderwrap blank shape is used in forming analysis for precise initial contacts between punch and blank. An adaptive mesh method is used in springback analysis for precise calculation of bending moments. In springback analysis, the differences of 2 and 3 dimensional analysis are compared and the effects of blank holdig force and friction coefficient are evaluated. In order to verify the validity of simulation results, they are compared with measured ones. The predicted thickness distribution and formed shape are agreed well with those of the measurement. The Predicted springback amount is less than that of the measurement.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2004년도 추계학술대회논문집
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• pp.124-127
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• 2004

In the previous experimental study about extrusion of circular product with four helical fins, it was known that product with helical fins may not to be rotated during extruding with rotating extrusion dies in spite of using twisted dies. According to the results of experiments with Plasticin material, it was anticipated that the extrusion load could be reduced if rotating dies could be used, because it needs high pressure in order to twist billet and form fin shape on the surface of product in the case of using conventional fixed helical dies. So, in this paper, according to the extrusion load analyzed by DEFORM-3D software, optimal rotational velocity of rotating dies can be obtained, and the twisting, angle of product can be analyzed during extruding product with helical fins in the case of two types of rotating of dies. The results of analysis by DEFORM-3D show that the twisting angle of product can be controlled by twisted angle of extrusion helical dies and the rotational velocity of helical dies.

• 한국해양환경ㆍ에너지학회지
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• 제14권2호
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• pp.114-120
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• 2011

조류발전용 다리우스 터빈의 변형된 형태인 헬리컬 터빈의 설계 인자 변화에 따른 성능을 수치해석으로 살펴보았다. 헬리컬 터빈은 수직축 다리우스 터빈을 회전축을 중심으로 상부와 하부를 비틀리게 함으로써 다리우스 터빈의 일반적인 취약점인 초기구동불량과 진동문제를 개선하기 위해 고안된 형태이다. 본 논문에서는 헬리컬 터빈의 비틀림각(Twisting Angle)과 직경대비 높이를 변화시키며 수치해석을 수행하였고, 결과를 바탕으로 최적의 구조를 제안하였다. 3차원 비정상 난류유동해석을 위하여 FLUENT의 RANS방정식과 k-${\omega}$ SST 난류모델을, 격자계 모델링을 위하여 GAMBIT을 이용하였다. 헬리컬 터빈은 적절한 비틀림각에서 양호한 발전효율을 보장하면서 진동을 유발하는 회전력 변화의 진폭을 최소화 할 수 있음을 확인하였고, 효율의 최대가 확보되는 터빈의 최소 높이를 발견하였다.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1998년도 춘계학술대회논문집
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• pp.210-213
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• 1998

A kinematically admissible velocity field is developed for the analysis of twisting of extruded products. The twisting of extruded product is caused by the linearly increased rotational velocity from the center on the cross-section of the workpiece at the die exit. In the analysis, the rotational velocity in angular direction is assumed by the multiplication of radial distance and angular velocity. The angular velocity is zero at the die entrance and is increased linearly by axial distance from die entrance. The increase rate of angular velocity is determined by the minimization of plastic work. The results of the analysis show that the angular velocity of the extruded product increase with the die twisting angle and the aspect ratio of product and friction condition and reduction area and show that angular velocity increases with the decreases in die length.

• 소성∙가공
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• 제14권5호
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• pp.444-451
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• 2005

A new extrusion process of the circular section product with helical fins could be developed by rotating extrusion die. The twisting of extruded product is caused by the twisted conical die surface connecting the die entrance section and the die exit section linearly. But, until now, because the process has used fixed extrusion die, it needs high pressure in order to twist billet and form fin shape on the surface of billet. So, during extruding billet, in order not to twist billet, the extrusion die is needed to rotate itself instead of twisting of billet. It is known that it is possible to reduce extrusion load of product with helical fins by analysis and experiments using rotating die. And it is known that, through the extrusion load analysis by $DEFORM^{TM}-3D$ software, optimal rotational velocity of rotating die can be obtained according to reduction ratio of area and twisted angle of die. And experiments and analysis using rotating extrusion die show that the twisted angle of product can be controlled by twisted angle of extrusion helical die and the rotational velocity of extrusion helical die.

• 국제초고층학회논문집
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• 제3권3호
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• pp.223-230
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• 2014

In this study the progressive collapse resisting capacities of tall diagrid buildings were evaluated based on arbitrary column removal scenario, and the seismic load-resisting capacities were investigated through fragility analysis and ATC 63 procedure. As analysis model structures both regular and twisted diagrid structures were designed and their load-resisting capacities were compared by nonlinear static and dynamic analyses. The analysis results showed that the progressive collapse potential of twisted buildings decreased as the twisting angle increased, but the seismic fragility or the probability of failure decreased as the twisting angle increased.

• 한국항공우주학회지
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• 제34권3호
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• pp.14-21
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• 2006

직사각형 평판날개의 날개짓과 비틀림 운동을 해석하기 위하여 비정상 와류격자법(VLM)을 이용하였다. 단순 상하 및 피칭 운동하는 날개에 대한 해석결과를 실험 및 다른 수치해석 결과들과 비교하여 복잡한 날개짓 비행을 모사하는데 본 방법을 사용할 수 있음을 보였다. 날개짓 각 진폭이 $20^{\circ}$인 경우에 여러 가지 비틀림 각과 무차원 주파수 변화에 대하여 직사각형 평판 날개의 양력, 추력 및 추진효율을 계산하였다. 계산 결과를 분석하여 주기적으로 변하는 비틀림이 날개짓 날개의 공력 특성에 미치는 영향을 살펴보았다.