• International Journal of Naval Architecture and Ocean Engineering
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• 제11권2호
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• pp.883-898
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• 2019

This paper employs computational tools to predict power increase (or speed loss) and propulsion performances in waves of KVLCC2. Two-phase unsteady Reynolds averaged Navier-Stokes equations have been solved using finite volume method; and a realizable k-ε model has been applied for the turbulent closure. The free-surface is obtained by solving a VOF equation. Sliding mesh method is applied to simulate the flow around an operating propeller. Towing and self-propulsion computations in calm water are carried out to obtain the towing force, propeller rotating speed, thrust and torque at the self-propulsion point. Towing computations in waves are performed to obtain the added resistance. The regular short head waves of λ/LPP = 0.6 with 4 wave steepness of H/λ = 0.007, 0.017, 0.023 and 0.033 are taken into account. Four methods to predict speed-power relationship in waves are discussed; Taylor expansion, direct powering, load variation, resistance and thrust identity methods. In the load variation method, the revised ITTC-78 method based on the 'thrust identity' is utilized to predict propulsive performances in full scale. The propulsion performances in waves including propeller rotating speed, thrust, torque, thrust deduction and wake fraction, propeller advance coefficient, hull, propeller open water, relative rotative and propulsive efficiencies, and delivered power are investigated.

• 한국항공우주학회지
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• 제47권3호
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• pp.204-211
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• 2019

희박연료 직접분사(Lean Direct injection(LDI)) 가스터빈 연소기에 대한 이상유동 특성을 해석하였다. LDI 연소기에 적용된 환형분사기(hollow-cone spray injector)의 분열을 모사하기 위해 분열모델(Linearized Instability Sheet Atomization(LISA), Aerodynamically Progressed Taylor Analysis Breakup(APTAB)을 적용하였다. 침투깊이와 평균입도(Sauter Mean Diameter(SMD))를 통해 분열모델을 검증하였으며, LDI 연소기에 적용하여 이상유동특성을 분석하였다. 스월인젝터로 인해 Precessing Vortex Core(PVC)가 발생하였으며, 액적들이 PVC를 따라 미립화되는 것을 확인하였다. SMD 결과를 통해 PVC가 회전하는 영역의 외곽으로 즉, 빠른 속도 영역에 액적들이 분포하며, 스톡스수(Stokes number)는 1보다 작다.

• 한국항공우주학회지
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• 제47권4호
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• pp.256-265
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• 2019

본 논문에서는 평직물 CFRP로 제작한 직교 격자 쉘의 굽힘 하중에 의한 점진적 손상 연구를 수행하였다. 직교 격자는 복합재 바닥면과 함께 경화하여 제작하였다. 굽힘을 받는 직교 격자 쉘의 점진적 손상 해석은 Hashin-Rotem 파손 기준과 Matzenmiller-Lubliner-Taylor (MLT) 모델으로 비선형 유한요소법을 이용하여 수행하였다. 또한, 직교 격자 쉘에 대한 3점 굽힘 시험을 수행하였으며, 시험 결과와 해석 결과를 비교하였다. 변형률과 변위에 대한 시험과 해석 결과는 유사하게 나타났다. 손상 영역은 점진적 손상 해석으로 예측하였으며, 육안 검사와 초음파 비파괴 검사를 통해 측정한 결과와 비교하였다.

• 한국추진공학회지
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• 제26권2호
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• pp.1-11
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• 2022

일반적인 축소 확대형 초음속 노즐에 대한 열해석에서 경계조건으로 사용되는 벽면의 열전달 계수는 노즐 전체의 열해석 정확도에 영향을 미친다. 이에 많은 열전달계수 도출 방법이 제안되어 왔으며, 본 연구에서는 각각의 기법들을 실제 실험 조건에서 열전달 계수를 계산하고 비교하고자 하였다. 이를 위해 기 수행된 벽면 등온 노즐의 열전달실험에 대해 이론 기반의 analogy 기법과 반경험식, 유체전산해석을 통해 열전달 계수를 도출하고 실험결과와 비교하였다. 해석 결과는 반경험식들은 전반적으로 다른 방법에 비해 대류 열전달 계수를 과도하게 예측하고, Prandtl-Taylor analogy 기법과 k-ω SST 모델을 적용한 전산해석 결과가 실험결과와 비교적 잘 일치하는 경향성을 보였다.

• 한국CDE학회논문집
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• 제18권5호
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• pp.359-366
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• 2013

In the lower arm design process, a tolerance optimization of the variance of design variables should be preceded before manufacturing process, since it is very cost-effective compared to a strict management of tolerance of products. In this study, a design of experiment (DOE) based on response surface model (RSM) was carried out to find optimized design variables of the lower arm, which can meet a given requirement of probability constraint for the process capability index (Cpk) of the weight and maximum stress. Then, the design space was explored by using the central composite design method, in which the 2nd order Taylor expansion was applied to predict a standard deviation of the responses. The optimal solutions satisfying the probability constraint of the Cpk were found by considering both of the mean value and the standard deviation of the design variables.

• Nuclear Engineering and Technology
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• 제43권5호
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• pp.447-458
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• 2011

This paper proposes an approximated contact force model to identify the nonlinear behavior of a fuel rod with gap supports; also, the numerical prediction of interfacial forces in the mechanical contact of fuel rods with gap supports is studied. The Newmark integration method requires the current status of the contact force, but the contact force is not given a priori. Taylor's expansion can be used to predict the unknown contact force; therefore, it should be guaranteed that the first derivative of the contact force is continuous. This work proposes a continuous and differentiable contact force model with the ability to estimate the current state of the contact force. An approximated convex and differentiable potential function for the contact force is described, and a variational formulation is also provided. A numerical example that considers the particularly stiff supports has been studied, and a fuel rod with hardening supports was also examined for a realistic simulation. An approximated proper solution can be obtained using the results, and abrupt changes from the contacting state to non-contacting state, or vice versa, can be relieved. It can also be seen that not only the external force but also the developed contact force affects the response.

• 대한조선학회논문집
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• 제36권2호
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• pp.121-134
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• 1999

본 논문에서는 유체 정역학적 계산, 용적 계산, 비손상 및 손상시 복원성 그리고, 선형 변환을 수행할 수 있는 객체 지향적 선박계산 전산프로그램을 개발하였다. 선박 계산을 위한 선형과 구획 형상을 NURBS(Non-Uniform Rational B-Spline) curve wire-frame model로 표현하고, 선형과 구획 단면 형상을 직접 3차원 평면과의 교차 계산을 통해 유체 정역학적 계산과 용적 계산을 수행하였다. 선박의 3차원 정역학적 평형 상태 방정식을 정식화하고, 순차적으로 선형화하여 힘과 모멘트 평형상태의 자세를 구하였다. 상용 선박 계산 프로그램의 결과와 비교하여, 개발 프로그램을 쉽고, 편리하게 사용할 수 있고, 계산의 정확도가 높음을 확인할 수 있었다.

• 대한조선학회논문집
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• 제51권2호
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• pp.154-161
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• 2014

Naval ships have hull appendages which are more exposed to the outside because of its small block coefficient compared with commercial ships. These exposed hull appendages like skeg, strut and shaft line affect the maneuverability of a ship. The effect of hull appendages has considered at initial design stage to estimate more accurate maneuverability. In this paper, sensitivity analysis is used to analyze the effect on maneuverability by hull appendages. 3 DOF maneuvering equations based on Mathematical Modelling Group (MMG) model are used and propeller & rudder model are modified to reflect the characteristics of twin propeller & twin rudder. Numerical maneuvering simulations (Turning test, Zig-zag test) for benchmark naval vessel, David Taylor Model Basin (DTMB) 5415 are performed. In every simulation, it is calculated that stability indices and maneuverability characteristics (Tactical Dia., Advance, 1st Overshoot, Time of complete cycle) with respect to the parameters (area times lift coefficient slope, attachment location) of hull appendages. As a result, two regression formulas are established. One is the relation of maneuverability characteristics and stability indices and the other is the relation of stability indices and hull appendages.

• KDI Journal of Economic Policy
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• 제36권2호
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• pp.1-64
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• 2014

본고는 소규모 개방경제를 상정한 동태확률모형을 통해 2000년 이후의 한국 거시경제의 변동요인들과 금융위기 기간의 통화정책과 재정정책의 변화요인을 추정하였다. 실증분석을 위해 동태확률모형은 경제성장률을 결정하는 두 가지 다른 추세요인과 다양한 구조충격요인 그리고 다양한 형태의 마찰을 포함시킴으로써, 거시변수들이 어떠한 요인에 의해 변화했는지를 정량적으로 분석하였다. 실증분석 결과, 금융위기 기간 동안 통화정책은 주로 테일러 준칙을 따른 것으로 나타난 반면, 재정정책의 반응은 재정준칙보다는 상대적으로 큰 폭의 재정충격요인에 의해서 설명된 것으로 추정되었다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제10권2호
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• pp.212-224
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• 2018

The characteristics of the relationship between the evolution of propeller trailing vortex wake and skew angle are numerically examined based on four different five-blade David Taylor Model Basin (DTMB) model propellers with different skew angles. Numerical simulations are based on Reynolds-averaged Naviere-Stokes (RANS) equations combined with SST $k-{\omega}$ turbulence model. Results show that the contraction of propeller trailing vortex wake can be restrained by increasing skew angle and loading conditions, and root vortices fade away when the propeller skew angle increases. With the increase of the propeller's skew angle, the deformation of the hub vortex and destabilization of the tip vortices are weakening gradually because the blade-to-blade interaction becomes weaker. The transition trailing vortex wake from stability to instability is restrained when the skew increases. Furthermore, analyses of tip vortice trajectories show that the increasing skew can reduce the difference in trailing vortex wake contraction under different loading conditions.