• International Journal of Aeronautical and Space Sciences
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• 제3권2호
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• pp.76-81
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• 2002

A numerical simulation of wake behavior behind three-dimensional wings in ground effect is done using an indirect boundary element method (Panel Method). An integral equation is obtained by applying Green's 2nd Identity on all surfaces of the flow domain. The AIC is constructed by imposing the no penetration condition on solid surfaces, and the Kutta at the wing's trailing edge. The ground effect is included using an image method. At each time step, a row of wake panels from wings' trailing edge are convected downstream following the force-free condition. The roll-up of wake vortices behind wings in close proximity is simulated.

• Journal of information and communication convergence engineering
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• 제12권1호
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• pp.39-45
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• 2014

A numerical method for solving Hamiltonian equations is said to be symplectic if it preserves the symplectic structure associated with the equations. Various symplectic methods are widely used in many fields of science and technology. A symplectic method preserves an approximate Hamiltonian perturbed from the original Hamiltonian. It theoretically supports the effectiveness of symplectic methods for long-term integration. Although it is also related to long-term integration, numerical stability of symplectic methods have received little attention. In this paper, we consider explicit symplectic methods defined for Hamiltonian equations with Hamiltonians of the special form, and study their numerical stability using the harmonic oscillator as a test equation. We propose a new stability criterion and clarify the stability of some existing methods that are visually based on the criterion. We also derive a new method that is better than the existing methods with respect to a Courant-Friedrichs-Lewy condition for hyperbolic equations; this new method is tested through a numerical experiment with a nonlinear wave equation.

• 충청수학회지
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• 제28권4호
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• pp.623-633
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• 2015

In this paper, a general Weighted Essentially Non-Oscillatory (WENO) interpolation is proposed and applied to a semi-Lagrangian method. The proposed method is based on the conservation law, and characteristic curves are used to complete the semi-Lagrangian method. Therefore, the proposed method satisfies conservation of mass and is free of the CFL condition which is a necessary condition for convergence. Using a several standard examples, the proposed method is compared with the third order Strong Stability Preserving (SSP) Runge-Kutta method to verify the high-order accuracy.

• Tribology and Lubricants
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• 제12권2호
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• pp.65-73
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• 1996

Rapid increase of Refrigeration and Air conditioning system in modem industries brings attention to the urgency of core technology development in the area. This paper presents theoretical investigation of the lubrication characteristics of rotary compressor for refrigeration and air conditioning. In order to analyze the lubrication characteristics of the main & sub bearing of rotary compressor, the bearing force and locus of shaft center are analyzed by the dynamic analysis of rotary compressor and numerical analysis of Reynolds equation as the operating condition is changed in various ways. In this paper, we used the Runge-Kutta method for the dynamic analysis of rotary compressor and the SOR (Successive OverRelaxation) method for the numerical analysis of Reynolds equation. The result shows that the operating condition of sub bearing is severer than that of main bearing, and eccentricity ratio grows as the bearing force increases. It is believed that the result can be applied to the design of alternative refrigerant rotary compressor.

• 한국소음진동공학회논문집
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• 제18권5호
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• pp.558-563
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• 2008

Vibration/shock affects biggest taking a train subtraction of vehicle and durability decline. Therefore, absorber is used for vibration/shock isolation and various qualities of the material and design are applied to isolation. This paper proposes vibration/shock absorber that applies 'Disc' spring. Through comparison with 'Disc' spring that has nonlinearity and coil spring that is having linearity, see effect that nonlinearity of isolation gets in vibration/shock Isolation. Coil spring and 'Disc' spring are non-linear numerical analysis and simulation through theory for this, get and investigate comparison result through an experiment finally. Expressed and formulated shock through 'Runge-Kutta' method/impact response to nonlinear-vibration-equation of 1 degree of freedom for numerical analysis. Double half sine pulse of excitation used and analyzed result through spectrum response analysis here. Response of disc spring is compared to response of coil spring by changing $h_o/t$ ratio with computer simulation and the usage of disc spring is increased through analysis of effect of design factors. The purpose of this paper is that the shock response of disc spring is calculated through numerical simulation and to design the optimal absorber under the limited condition. And then, the isolation effect was analyzed through the shock test.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 춘계학술대회논문집
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• pp.990-993
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• 2008

Vibration/shock affects biggest taking a train subtraction of vehicle and durability decline. Therefore, absorber is used for vibration/shock isolation and various qualities of the material and design are applied to isolation. This paper proposes vibration/shock absorber that applies 'Disc'spring. Through comparison with 'Disc' spring that has nonlinearity and coil spring that is having linearity, see effect that nonlinearity of isolation gets in vibration/shock isolation. Coil spring and 'Disc' spring are non-linear numerical analysis and simulation through theory for this, get and investigate comparison result through an experiment finally. Expressed and formulated shock through 'Runge-Kutta' method/impact response to nonlinear-vibration-equation of 1 degree of freedom for numerical analysis. Double half sine pulse of excitation used and analyzed result through spectrum response analysis here. Response of disc spring is compared to response of coil spring by changing ho/t ratio with computer simulation and the usage of disc spring is increased through analysis of effect of design factors. The purpose of this paper is that the shock response of disc spring is calculated through numerical simulation and to design the optimal absorber under the limited condition. And then, the isolation effect was analyzed through the shock test.

• 융합정보논문지
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• 제10권7호
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• pp.131-137
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• 2020

가진 정현파 강제력에 의한 강제 진동의 특성이 연구되었고 또한, 주파수 영역에서 FRF의 수치 분석을 자세히 수행하였다. 이와 관련하여 강제 진동 모델에서 변위, 속도 및 가속도의 응답을 구하였다. 고유 주파수 주변의 실수부와 허수부의 FRF 특성도 각 경우에 따라 구하였다. 시간 영역에서의 강제 진동의 응답분석은 정현파 강제 진동의 특성을 식별할 수 있다. 변위, 속도 및 가속도 등의 응답을 얻기 위해 Runge-Kutta-Gill 방법의 수치해석 기법을 수행하여 강제력 주파수에 따른 응답을 얻었고 이 주파수는 응답에 큰 영향을 미치지 않았다. 또한, FRF는 강제 진동의 고유 특성을 나타내고 있으며 이러한 강제 진동 모델의 각 감쇠 조건에서 이러한 응답분석을 성공적으로 자세하게 얻을 수 있었다. 상이한 질량, 감쇠 및 강성에 대한 수치 분석 후, 정현파 강제력에 의한 강제 진동 응답 특성을 강제력의 진폭 및 주파수를 동시에 고려하여 분석되었다.

• 대한토목학회논문집
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• 제43권2호
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• pp.187-193
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• 2023

이 논문은 말뚝체의 자중을 고려한 말뚝의 좌굴거동에 관한 연구이다. 비균질 지반에 설치된 부분매립 말뚝의 좌굴을 지배하는 미분방정식과 경계조건을 유도하였다. Runge-Kutta법과 Regula-Falsi법을 결합한 수치해석법을 적용하여 말뚝의 좌굴하중과 좌굴형을 산정하였다. 계산된 좌굴하중의 수치해와 문헌값은 잘 일치하였고, 수치예를 통해 말뚝의 자중, 매립비, 세장비, 경계조건 및 지반의 반력형상비, 지반강성비가 말뚝의 좌굴특성에 미치는 영향을 분석하였다. 분석결과, 말뚝의 자중은 말뚝의 좌굴하중을 감소시켰으며 이러한 자중효과의 무시는 부분매립 말뚝의 좌굴하중을 과대평가할 수 있음을 확인하였다.

• 한국해안·해양공학회논문집
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• 제36권2호
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• pp.70-79
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• 2024

본 연구에서는 3차원 공간에서 바닥의 움직임에 따른 선형파의 생성을 모의할 수 있는 스펙트럼 법을 소개한다. 지배방정식은 선형의 동역학적 및 운동학적 자유수면 경계조건이며, 두 식은 Fourier 공간에서 해석된다. 해석된 속도포텐셜 및 자유수면변위는 연속방정식과 운동학적 바닥경계조건을 항상 만족해야 한다. 수치해석에서 시간 적분은 4차 Runge-Kutta 법을 이용하여 해석하였다. Fourier 공간에서 해석한 결과는 Fourier 역변환을 통해 실제 공간에서의 속도포텐셜과 자유수면변위로 표현된다. 본 수치모델을 이용하여 다양한 형상의 바닥이 규칙적으로 움직이는 경우 생성되는 규칙파에 대해 모의하였다. 또한 바닥의 움직임을 이용하여 비스듬히 전파하는 규칙파의 생성도 모의하였다. 수치모델의 결과는 해석해와 비교하였으며, 거의 일치하는 결과를 보였다.

• 한국공간구조학회논문집
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• 제20권2호
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• pp.59-68
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• 2020

In this paper, the dynamic snapping of the 3-free-nodes spatial truss model was studied. A governing equation was derived considering geometric nonlinearity, and a model with various conditions was analyzed using the fourth order Runge-Kutta method. The dynamic buckling phenomenon was observed in consideration of sensitive changes to the force mode and the initial condition. In addition, the critical load level was analyzed. According to the results of the study, the level of critical buckling load elevated when the shape parameter was high. Parallelly, the same result was caused by the damping term. The sensitive asymmetrical changes showed complex orbits in the phase space, and the critical load level was also becoming lowly. In addition, as the value of damping constant was high, the level of critical load also increases. In particular, the larger the damping constant, the faster it converges to the equilibrium point, and the occurrence of snapping was suppressed.