• Nuclear Engineering and Technology
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• 제54권10호
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• pp.3745-3765
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• 2022

The concrete structures related to nuclear safety are threatened by accidental impact loadings, mainly including the low-velocity drop-weight impact (e.g., spent fuel cask and assembly, etc. with the velocity less than 20 m/s) and high-speed projectile impact (e.g., steel pipe, valve, turbine bucket, etc. with the velocity higher than 20 m/s), while the existing studies are still limited in the impact resistant design of nuclear power plant (NPP), especially the primary RC slab. This paper aims to propose the numerical simulation and theoretical approaches to assist the impact-resistant design of RC slab in NPP. Firstly, the continuous surface cap (CSC) model parameters for concrete with the compressive strength of 20-70 MPa are fully calibrated and verified, and the refined numerical simulation approach is proposed. Secondly, the two-degree freedom (TDOF) model with considering the mutual effect of flexural and shear resistance of RC slab are developed. Furthermore, based on the low-velocity drop hammer tests and high-speed soft/hard projectile impact tests on RC slabs, the adopted numerical simulation and TDOF model approaches are fully validated by the flexural and punching shear damage, deflection, and impact force time-histories of RC slabs. Finally, as for the two low-velocity impact scenarios, the design procedure of RC slab based on TDOF model is validated and recommended. Meanwhile, as for the four actual high-speed impact scenarios, the impact-resistant design specification in Chinese code NB/T 20012-2019 is evaluated, the over conservation of which is found, and the proposed numerical approach is recommended. The present work could beneficially guide the impact-resistant design and safety assessment of NPPs against the accidental impact loadings.

• 한국시뮬레이션학회논문지
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• 제19권4호
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• pp.1-9
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• 2010

본 논문에서는 여객선의 승객 비상 탈출 시뮬레이션을 구현하였다. 승객의 행동에 미치는 요인 중 연령, 성별을 고려하여 승객 개인의 보행 속도에 반영하는 속도 기반 모델을 사용하였다. 승객들의 집단 이동을 구현하기 위해 플로킹 알고리즘을 적용하였다. 장애물과의 충돌 회피 및 승객 간의 위치가 겹치는 현상을 방지하기 위해 페널티 보행 속도를 도입하였다. 이 알고리즘을 이용하여 여객선의 승객 탈출 규정인 IMO (International Maritime Organization) MSC (Maritime Safety Committee) Circ.1238에서 정의한 11가지 시험 문제에 적용하였다. 시험 문제를 통해 승객의 위치가 겹치는 현상이 없이 시뮬레이션 되는 것을 확인하였다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제11권1호
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• pp.119-130
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• 2019

This paper establishes an iterative calculation model for the hydrodynamic performance of propeller in oblique flow based on low order potential based surface panel method. The hydrodynamic performance of propeller is calculated through panel method which is also used to calculate the induced velocity. The slipstream of propeller is adjusted according to the inflow velocity and the induced velocity. The oblique flow is defined by the axial inflow velocity and the incident angle. The calculation results of an instance show that the thrust and torque of propeller decrease with the increase of axial inflow velocity but increase with the incident angle. The unsteadiness of loads on the propeller blade surface gets more intensified with the increases of axial inflow velocity and incident angle. However, comparing with the effect of axial inflow velocity on the unsteadiness of the hydrodynamic performance of propeller, the effect of the incident angle is more remarkable.

• Steel and Composite Structures
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• 제26권6호
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• pp.771-791
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• 2018

This paper deals with the low velocity impact response and dynamic stresses of composite sandwich truncated conical shells (STCS) with compressible or incompressible core. Impacts are assumed to occur normally over the top face-sheet and the interaction between the impactor and the structure is simulated using a new equivalent three-degree-of-freedom (TDOF) spring-mass-damper (SMD) model. The displacement fields of core and face sheets are considered by higher order and first order shear deformation theory (FSDT), respectively. Considering continuity boundary conditions between the layers, the motion equations are derived based on Hamilton's principal incorporating the curvature, in-plane stress of the core and the structural damping effects based on Kelvin-Voigt model. In order to obtain the contact force, the displacement histories and the dynamic stresses, the differential quadrature method (DQM) is used. The effects of different parameters such as number of the layers of the face sheets, boundary conditions, semi vertex angle of the cone, impact velocity of impactor, trapezoidal shape and in-plane stresses of the core are examined on the low velocity impact response of STCS. Comparison of the present results with those reported by other researchers, confirms the accuracy of the present method. Numerical results show that increasing the impact velocity of the impactor yields to increases in the maximum contact force and deflection, while the contact duration is decreased. In addition, the normal stresses induced in top layer are higher than bottom layer since the top layer is subjected to impact load. Furthermore, with considering structural damping, the contact force and dynamic deflection decrees.

• 천문학회보
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• 제40권1호
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• pp.42.3-43
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• 2015

Using a large sample of 32,000 type 2 AGNs out to z = 0.2, we present the statistical results on the ionized gas outflows, based on the analysis of the velocity shift of narrow emission lines with respect to the systemic velocity measured from the stellar absorption lines. Considering the projection effect, the fraction of type 2 AGNs with the [O III] velocity offset, which is ~50%, is comparable to that of type 1 AGNs. The velocity dispersion of [OIII] is typically larger than that of Ha, suggesting that outflow is prevalent in type 2 AGNs. A weak correlation of the OIII luminosity with velocity shift and velocity dispersion indicates that outflow velocity is stronger for higher luminosity AGNs. Based on our 3-D biconical outflow models with simple assumptions on the velocity structure, we simulate the projected 2-D velocity and velocity dispersion maps, which are spatially integrated to reproduce the measurements of SDSS AGNs. By comparing the distribution of the measured velocity and velocity dispersion of OIII, with the model grids, we constrain the intrinsic outflow velocities. The outflow velocity ranges from a few hundreds to a thousand km/s, implying a strong feedback to ISM.

• 제어로봇시스템학회논문지
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• 제7권2호
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• pp.109-116
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• 2001

The paper presents a speed control algorithm for a full pitch-controlled wind turbine system. Torque of a blade generated by wind energy is a nonlinear function of wind speed, angular velocity, and pitch angle of the blade. The design of the controller, in general, is performed by linearizing the torque in the vicinity of the operating point assuming the angular velocity of the blade is constant. For speed control, however the angular velocity is on longer a constant, so that linearization of the torque in terms of wind speed and pitch angle is impossible. In this study, a reference pitch model is derived in terms of a wind speed, angular velocity, and pitch angle, which makes it possible to design a controller without linearizing the nonlinear torque model of the blade. This paper also suggests a method of designing a hydraulic control system for changing the pitch angle of the blade.

• Journal of Advanced Marine Engineering and Technology
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• 제26권6호
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• pp.670-678
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• 2002

Fluid flow in a rectangular duct with $90^{\circ}$ mitered elbow is measured by 5W laser doppler velocity meter. The fluid flow is also computed by commercial software of STAR-CD for comparison between measured and computed velocity profiles in the duct. Reynolds numbers for the comparison are 1,608 and 11,751 based on mean velocity and hydraulic diameter of the duct. First, the fluid flow of Reynolds number equal to 1,608 is predicted by assumptions of both laminar and turbulent models. But, even though the Reynolds number is less than 2,300~3,000, the computation by turbulent model is closed to the experimental data than that by laminar model. Second, the computation for Reynolds number of 11,751 by turbulent model also predicted the experimental data satisfactorily.

• Korean Chemical Engineering Research
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• 제61권3호
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• pp.446-455
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• 2023

공기부양반응기(airlift reactor) 내의 액체순환속도(liquid circulation velocity)를 예측하기 위한 수학적 모형이 유체순환고리(fluid circulation loop)에 대한 기계적 에너지 수지를 기초로 개발되었다. 그 모형은 90° 방향전환으로 인한 에너지 손실과 반응기의 각 부위에서의 마찰로 인한 에너지 손실 그리고 단면적의 변화로 인한 에너지 손실을 모두 고려하였다. 마찰과 방향전환 그리고 단면적 변화에 의한 손실계수를 각각 고려한 모형이 집중매개변수(lumped parameter)를 사용한 기존의 모형보다 액체순환속도를 더 잘 예측할 수 있었다. 순환액체속도는 추적자펄스방법(tracer pulse method)으로 측정하였다. 개발된 모형은 상하부에 연결관(connecting pipe)을 갖는 외부순환 공기부양반응기에서 얻은 본 연구의 실험 결과의 대부분은 물론이고 다양한 형태의 공기부양반응기에서 얻어진 다른 연구자들의 결과도 ±20%이내의 오차로 잘 예측할 수 있었다. 외부 및 내부순환 공기부양반응기에서 순환유체의 90° 방향전환과 관련된 손실계수에 대한 유용한 실험식을 구하여 액체순환속도를 예측하는 데 사용하였다.

• 산업기술연구
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• 제20권B호
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• pp.95-103
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• 2000

A model trains must have similitude with its original model not only in shape but also in motion. Motion characteristics of a model train under considerations are maximum velocity in straight and circular tracks and stopping distance. Equations of motions are derived to obtain maximum speed and stopping distance based on the Newton's Second Law and the energy principal. To accurately predict traction and resistance force between wheel and rail. wheel slip, or creepage, is taken into consideration. To verify the equations of motion, various experiments have been carried out including measurement of gear efficiency, location of mass center, rolling resistance force, traction force, slip, maximum velocity and stopping distance. This paper addresses how the experiments are setup and carried out in detail. Also the results of experiments are compared with the analytical prediction, which showed good agreements with each other.

• 한국수자원학회논문집
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• 제48권4호
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• pp.291-298
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• 2015

본 연구의 목적은 하천에서 흐름방향 유속의 횡분포식에 기반하여 1차원 종분산계수를 이론적으로 유도하고 이들의 타당성을 검증하는 것이다. 이를 위해 본 논문의 전편 "I. 흐름방향 유속의 횡포식"에서는 Shiono-Knight Model (일명 SKM)을 도입하여 삼각형 단면수로에서 횡분포식을 해석적으로 유도하였다. 본 논문의 후편 "II. 종분산계수"에서는 전편에서 유도된 유속의 횡분포식을 Fischer (1968)의 삼중 적분식에 대입하여 1차원 종분산계수 이론식을 새롭게 개발하였다. 본래 SKM은 Navier-Stokes 방정식을 근간으로 개발되어 주로 직선수로이면서 사다리꼴 단면이나 복단면 수로에 적용되어 왔지만, 본 연구에서는 사행으로인한 최심선의 변동을 고려할 수 있는 삼각형을 단면형상으로 가정하였다. 유도된 해석해를 검증하기 위해 자연하천에서 실측된 유속자료와 비교 분석하였다. 또한 유도된 횡분포식을 이용하여 단면평균유속을 산정하고, 이를 Manning의 유속식의 결과와 비교 검증하였다. 본 연구에서 개발한 이론식은 비록 유속의 횡분포를 경우에 따라서 섬세하게 재현하지는 못하더라도 조도계수를 포함한 몇 가지 기본적인 수리 및 지형자료만 측량한다면 유속의 관측없이 비교적 정확한 유속분포를 산출해 낼 수 있는 장점이 있었다.