• KSCE Journal of Civil and Environmental Engineering Research
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• v.28 no.4B
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• pp.413-419
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• 2008

In this study, we develop analytical solutions for long waves propagating over several types of axis-symmetric topographies where the water depth varies in an arbitrary power of radial distance. The first type is a cylindrical island mounted on a shoal. The second type is a circular island. To get the solution, the methods of separation of variables, Taylor series expansion and Frobenius series are used. Developed analytical solutions are validated by comparing with previously developed analytical solutions. We also investigate various cases with different incident wave periods, radii of the shoal, and the powers of radial distance.

• Nuclear Engineering and Technology
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• v.27 no.3
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• pp.418-426
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• 1995

설계의 신뢰성은 응력해석을 통하여 확인될 수 있으며, 해석결과는 대상 부품의 구조적 건전성을 입증하는 근거가 된다. 본 보고서는 ANSYS의 피로해석 모듈을 이용한 CANDU 6핵연료채널의 응력해석 및 ASME Code에 따른 해석 절차 개발을 소개하였다. 응력해석은 ASME Code Section III NB-3200 의 $\ulcorner$Design by Analysis$\lrcorner$에 기초한 해석절차에 따라 수행하였으며, 체계적인 해석을 위해 자료 처리용 ANSYS 매크로 및 FORTRAN 프로그램을 개발하였다. 해석은 각 조건에 따라 기계적응력과 열응력해석으로 분리하여 수행한 후 조합되었으며, ANSYS 피로해석 모듈을 이용하여 선정된 절점들의 기계적응력과 열응력의 합에 대한 최대응력강도범위를 계산하였다. 응력해석 결과, CANDU 6 핵연료채널의 구조적 건전성이 입증되었으며, ANSYS를 이용한 ASME Code해석절차가 확립되어 CANDU 원자로 해석의 신뢰성을 크게 향상 시켰음은 물론 독자적인 수행을 위한 발판을 마련하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.8 no.2
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• pp.102-114
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• 2004

The present work has been developed the interpretation processor including the behavior of material failure and the separation phenomena under transient dynamic loading (the operation of explosive bolt) using AUTODYN V4.3, SoildWork 2003 and TrueGrid V2.1 programs. It has been demonstrated that the interpretation in ridge-cut explosive bolt under dynamic loading condition should be necessary to the appropriate failure model and the basic stress of bolt failure is the principal stress. The use of this interpretation processor developing the present work could be extensively helped to design the shape and the amount of explosives in the explosive bolt having a complex geometry. It is also proved that the interpretation processor approach is an accurate and effective analysis technique to evaluate the separation mechanism in explosive bolts.

• The Korean Journal of Rheology
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• v.10 no.2
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• pp.65-73
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• 1998

본연구에서는poystyrene-block-poly (ethlene-co-butylene)-block-polystyrene(SEBS) 삼중블록 공중합체와 저분자량 단일중합체인 Hercotac 1149 (H1149)의 70/30 (w/w) 혼합물 의 미세상분리와 그동력학을 유변물성 측정법과 SAXS 실험을 통하여 연구해 보았다. 먼저 혼합물의 미세상분리 온도를 유변물성 측정법과 SAXS 실험을 통해 각각구한 다음 샘플을 미세상분리 온도보다 높은 온도에서 그이하의 온도로 급냉시킨 후 유변물성과 산란강도의 사간에 따른 변화로부터 미세상분리 동력학에 대한 정보를 구하였다. 이렇게 얻어진 데이터 를 Avrami 형태의 핵생성 성장(NG) 메커니즘으로 해석해 보았는데 최대산란강도 Imax 뿐만 아니라 저장 점탄성계수 G＇과 손실 점탄성계수 G＂의 시간에 따른 변화를 잘 예측할수 있 었다. 한편 서로다른 두 time-resolved 실험으로부터 Avrami 플롯을 그려서 구해진 Avrami 변수들은 같은 급냉 깊이에서는 서로 잘 일치함을 확인하였다. 반감기는 급냉 깊이가 증가 함에 따라 점차 감소하는 경향을 보였는데 이는 급냉 깊이가 클수록 미세상분리가 더 빨리 진행되고 있음을 보여주는 것이다. 또한 Avrami 지수는 급냉 깊이가 증가함에 따라 3에서 4로 급격히 변했는데 이로부터 급냉 깊이가 작을 때에는 70/30 (w/w) SEBS/H1149 혼합물 의 미세상분리가 불균일 핵생성 성장 메커니즘에 따라 진행되고 급냉 깊이가 더 커지면 미 세상분리가 스피노달 상분리 메커니즘으로 변하고 있음을 예측할수 있었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2001.04a
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• pp.76-79
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• 2001

SIMULINK^{$\circledR}$를 이용하여 항공기용 터보프롭 엔진을 모델링한 후 현재 KT-1의 추진기관인 PT6A-62 분리축 터보프롭엔진의 성능을 해석하였다. SIMULINK^{$\circledR}$ 모델의 검증을 위하여 상용해석프로그램인 GASTURB 와 비교한 결과 최대오차율 1.07% 이내로 확인되었다. 지상정지 조건에서 블리드 공기유량을 0에서 5%, 보기류 구동에 따른 출력손실을 0에서 20 hp로 가정하고 해석한 결과 축마력은 최대 0.68%감소하며 비연료소모율은 거의 영향을 받지 않음을 알 수 있었다.

• Journal of Fisheries and Marine Sciences Education
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• v.6 no.2
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• pp.117-129
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• 1994

본 논문에서는 접촉하는 두 물체의 동적접촉문제를 해석하기위한 음해법과 양해법을 합성한 새로운 하이브리드 해석방법을 제안하였다. 그리고 양해법의 결과를 기준으로 하여 그 계산정도를 비교하고 제안한 방법의 정도와 효율의 유효성을 조사하였다. 얻어진 결과를 요약하면 아래와 같다. 1) 마찰을 고려한 음해법과 양해법의 정식화를 통하여 접촉상태에서 분리가 일어날때 까지를 표현할 수 있는 새로운 알고리즘을 제시하였다. 2) 본 방법은 종래의 음해법에 비해 계산시간이 짧고 계산정도는 거의 비슷한 결과를 보였다. 3) 하이브리드법은 알고리즘의 변경이 간단하고, 동적접촉문제의 해석을 위한 실용적인 면에 큰 장점을 가지고 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.130-134
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• 2006

The injection uniformity of the fuel manifold in a liquid rocket engine has been analyzed with dividing plates to improve the cooling performance at the face plate. Three dimensional computational fluid dynamics analysis has been performed to compare the injection uniformity for 5 candidate designs and has been verified to compare with the measured data for the optimal manifold design. For the case I and II, the coolant mass flux increases as the whole working fluid is enforced to flow under the dividing plate. The injection uniformity decreases due to the variation of mass flux at the end of dividing plate and the concentration of mass flow rate at the center of manifold. However case III and IV have uniform injection performance due to reduced mass flux concentration as the coolant can flow along both upper passage and lower passage of the dividing plate. Among the candidate designs, case IV is thought to be the optimal dividing plate with regard to cooling performance and injection uniformity.

• Journal of the Korean Crystal Growth and Crystal Technology
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• v.13 no.3
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• pp.145-151
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• 2003

Using computational fluid dynamics (CFD) method, we investigated three-dimensional fluid flow field and particle movement with respect to the injected gas flow rate variation in typical cyclone separator system. The results of numerical investigation were deduced by coupling the analysis of fluid flow field with Wavier-stokes equation and the tracking of the particle trajectory with Langrangian approach. It was shown that the increasing of injected gas flow rate resulted in the increasing of pressure loss in the separator. This change of inner pressure had an effect on an aspect of the fluid flow in the separator. Particle movement was determined by fluid flow in the separator and was fully depended on a diameter of particles under the fixed flow rate. Increasing of injected gas flow rate was led to an increasing of the trace of particle, so the particles moved to the lower part of the separator. For this reason, the minimum diameters of the particles were decreased and increased the separation rate under the fixed particle diameter. In conclusion, the changes of injected gas flow rate have an important factor to the fluctuation of the fluid flow field and particle trajectory in the separator.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.4
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• pp.269-275
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• 2020

An explosive bolt is one of many representative pyrotechnic release devices that separates two joined structures using explosives inside the bolt. In this study, a 1/2 inch ridge-cut explosive bolt with an EBW detonator was developed for usage in sled tests. The initial shape design was carried out based on the design method, and the performance test showed that the separation performance was outstanding but fragments occurred. Therefore, numerical analysis was performed to reduce the amount of debris by minimizing the amount of explosives. From the numerical analysis, the separation mechanism and characteristics of the ridge-cut explosive bolts were identified, and the minimum amount of explosives that does not generate debris was proposed. Verification tests revealed that the ridge-cut explosive bolts with the proposed explosive weight minimized fragments while maintaining the separation performance.

• Applied Chemistry for Engineering
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• v.22 no.6
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• pp.703-710
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• 2011

As the spacer in the membrane module provide the channel space to flow the feed solution smoothly and induce the flow turbulence, it could help to reduce both the concentration polarization and to take the long-term operation of membrane modules with high permeate flux by mixing the accumulated contaminants on the membrane surface into the bulk solution. In this study, the concentration distribution in membrane module with respect to the spacers which have the cross-sectional shapes of circle, cross, diamond and hexagon, the angles of spacer configuration, solute rejection and permeate flux were interpreted and optimized numerically using the "COMSOL Multiphysics" software. The concentration on the membrane surface was kept the lowest level for the cross-shape among the above four types of spacers. Also the 30 degree spacer configuration was showed as the most efficient case. The concentrations on the membrane surface at the module outlet for without spacer and the cross shape with the 30 degree spacer configuration were 2.09 and 1.29 times higher than those at inlet, respectively. The reduction effect of concentration polarization increased rapidly as the permeate flux increased.