• 한국전산구조공학회논문집
• /
• 제14권3호
• /
• pp.329-337
• /
• 2001

본 연구에서는 무단변속시에 사용되며, 세 개의 유성기어로 구성된 복합유성기어가 기어의 회진시 비선형적인 기어의 강성과 감쇠를 고려하여 모델링 되었고, 복합유성기어의 운동 방정식이 유도되었다. 소음과 진동의 원인인 선기어의 중심궤적이 구하여진 상태방정식에 4차 룬게-쿠타 수치해석 방법을 수행함으로써 구하였다.

• 한국수소및신에너지학회논문집
• /
• 제30권3호
• /
• pp.260-268
• /
• 2019

The pyrolysis characteristics of pulverized coal particle was numerically analyzed with the drop tube furnace. Based on the simulated gas flow field in the drop tube furnace, the particle velocity, temperature and volatile evolution were calculated with the fourth order Runge-Kutta method. The effects of changes in reactor wall temperature and particle diameter on the pyrolysis behavior of coal particle were investigated. The particle heating rate was very sensitive to the reactor wall temperature and particle size, that is, the higher wall temperature and the smaller particle size resulted in the higher heating rate and the consequent quicker volatile evolution.

• Structural Engineering and Mechanics
• /
• 제68권3호
• /
• pp.325-334
• /
• 2018

The Nonlinear dynamic response of a sandwich plate subjected to the low velocity impact is theoretically and experimentally investigated. The Hertz law between the impactor and the plate is taken into account. Using the Extended High Order Sandwich Panel Theory (EHSAPT) and the Ritz energy method, the governing equations are derived. The skins follow the Third order shear deformation theory (TSDT) that has hitherto not reported in conventional EHSAPT. Besides, the three dimensional elasticity is used for the core. The nonlinear Von Karman relations for strains of skins and the core are adopted. Time domain solution of such equations is extracted by means of the well-known fourth-order Runge-Kutta method. The effects of core-to-skin thickness ratio, initial velocity of the impactor, the impactor mass and position of the impactor are studied in detail. It is found that these parameters play significant role in the impact force and dynamic response of the sandwich plate. Finally, some low velocity impact tests have been carried out by Drop Hammer Testing Machine. The results are compared with experimental data acquired by impact testing on sandwich plates as well as the results of finite element simulation.

• 유변학
• /
• 제11권2호
• /
• pp.122-127
• /
• 1999

일정한 표면 온도를 갖는 쐐기형 물체 주위를 지나는 미세 극성유체의 정상상태 층류유동에 대하여 고찰하였다. Falkner & Skan에 의하여 유도된 상사해법을 이용하여 유동방향의 비선형 경계층 방정식의 해를 구하였다. 4계 Runge-Kutta법을 사용하여 Pr 수가 1일 경우의 열전달 특성을 수치적으로 해석하였고, 물질 매개변수에 대한 영향을 고찰하였다. 경계층을 가로지르는 무차원 속도와 Nusselt 수의 분포는 쐐기형 물체 주위를 지나는 Newtonian 유체의 경우와 비교하였다. Pr 수가 1이고 일정한 쐐기각을 가질 경우 물질 매개변수 K값이 증가할수록 Newtonian 유체의 경우보다 미세 극성유체의 경우 경계층의 두께가 증가하는 결과를 보였다. 그러나 물질매개변수 K값이 일정할 경우, Newtonian 유체보다 미세 극성유체의 열전달율이 더 작은 경향을 나타내었다.

• 한국항공우주학회지
• /
• 제38권10호
• /
• pp.973-978
• /
• 2010

본 논문에서는 유격을 고려한 항공기 전방 착륙 장치의 쉬미 현상을 연구하였다. 쉬미는 항공기의 이착륙 시 랜딩기어가 주행도중 측방향과 조향방향으로 진동에 놓이는 현상이다. 이 현상은 스트럿의 낮은 강성, 랜딩기어 내부의 마찰과 유격, 휠의 불균형이나 마모된 부품 등으로 인해 발생하며, 항공기의 안정성을 저하시킨다. 유격은 비선형 요소이기 때문에 기술 함수로 선형화 하여 주파수 영역에서 안정성해석을 수행하였고, 4차 Runge - Kutta를 이용하여 시간영역에서 안정성해석을 수행하였다. 본 연구에서는 수치적인 해석법을 통해 쉬미현상의 선형 동특성과 비선형 동특성을 조사하였다. 유격을 고려한 비선형 수치 해석결과, 선형 임계속도보다 낮은 속도에서 제한주기진동이 발생하는 등, 유격으로 인해 쉬미 안정성이 저감되는 결과를 관찰하였다.

• 한국전산구조공학회논문집
• /
• 제31권2호
• /
• pp.87-95
• /
• 2018

이 논문에서는 스펙트럴 요소법과 외연적 시간적분법을 이용해 SH파의 전파 거동을 계산하는 수치해석 기법을 제시한다. 2차원 영역에서의 탄성파 해석을 위해 해석영역을 유한 영역으로 한정하고 파동이 반사되지 않도록 수치적 파동흡수 경계조건인 perfectly matched layer(PML)를 도입하였다. PML이 포함된 시간영역 파동방정식의 유한요소해법을 위해 스펙트럴 요소법을 적용하였고 Legendre- Gauss-Lobatto 수치적분법을 사용하여 질량행렬을 대각화하였다. 2차 미분방정식 시스템의 파동방정식을 1차 미분방정식 시스템으로 변환하였고 병렬화를 통한 탄성파 해석 성능의 최적화를 위해 외연적 시간적분법인 4차 Runge-Kutta 방법을 이용해 해석영역에서의 변위응답을 계산하였다. 2차원 해석영역에서 SH파의 전파 거동을 계산하는 수치예제를 통해 제시한 외연적 스펙트럴 요소법의 정확성을 검증하였고 PML로 인한 반사파의 감쇠효과를 확인하였다. 외연적 시간적분법을 통한 탄성파 해석 기법은 3차원 영역과 같은 대규모 문제에서의 탄성파 수치해석을 효율적으로 수행할 수 있을 것으로 기대된다.

• Advances in aircraft and spacecraft science
• /
• 제7권4호
• /
• pp.291-308
• /
• 2020

In this paper, a numerical method is utilized to study the effect of a new vibration absorber on vibration response of the stiffened functionally graded (SFG) cylindrical shell under a couple of axial and transverse compressions. The material composition of the stiffeners and shell is continuously changed through the thickness. The vibration absorber consists of a mass-spring-damper system which is connected to the ground utilizing a linear local damper. To simplify, the spring element of the vibration absorber is called global potential. The von Kármán strain-displacement kinematic nonlinearity is employed in the constitutive laws of the shell and stiffeners. To consider the stiffeners in the model, the smeared stiffener technique is used. After obtaining the governing equations, the Galerkin method is applied to discretize the nonlinear dynamic equation of system. In order to find the nonlinear vibration responses, the fourth order Runge-Kutta method is utilized. The influence of the stiffeners, the dynamic absorber parameters on the vibration behavior of the SFG cylindrical shell is investigated. Also, the influences of material parameters of the system on the vibration response are examined.

• Steel and Composite Structures
• /
• 제26권4호
• /
• pp.453-461
• /
• 2018

In this paper, nonlinear vibrations of the unsymmetrical laminated composite beam (LCB) on a nonlinear elastic foundation are studied. The governing equation of the problem is derived by using Galerkin method. Two different end conditions are considered: the simple-simple and the clamped-clamped one. The Hamiltonian Approach (HA) method is adopted and applied for solving of the equation of motion. The advantage of the suggested method is that it does not need any linearization of the problem and the obtained approximate solution has a high accuracy. The method is used for frequency calculation. The frequency of the nonlinear system is compared with the frequency of the linear system. The influence of the parameters of the foundation nonlinearity on the frequency of vibration is considered. The differential equation of vibration is solved also numerically. The analytical and numerical results are compared and is concluded that the difference is negligible. In the paper the new method for error estimation of the analytical solution in comparison to the exact one is developed. The method is based on comparison of the calculation energy and the exact energy of the system. For certain numerical data the accuracy of the approximate frequency of vibration is determined by applying of the suggested method of error estimation. Finally, it has been indicated that the proposed Hamiltonian Approach gives enough accurate result.

• 정보저장시스템학회논문집
• /
• 제5권1호
• /
• pp.19-35
• /
• 2009

The present work is an experimental and analytical study on a flexible disk rotating close to a rigid rotating disk in open air. In the analytical study, the air flow in the gap between the flexible disk and the rigid disk is modeled using Navier-Stokes and continuity equations while the flexible disk is modeled using the linear plate theory. The flow equations are discretized using the cell centered finite volume method (FVM) and solved numerically with semi-implicit pressure-linked equations (SIMPLE algorithm). The spatial terms in the disk equation are discretized using the finite difference method (FDM) and the time integration is performed using fourth-order Runge-Kutta method. An experimental test-rig is designed to investigate the dynamics of the flexible disk when rotating close to a co-rotating, a counter-rotating and a fixed rigid disk, which works as a stabilizer. The effects of rotational speed, initial gap height and inlet-hole radius on the flexible disk displacement and its vibration amplitude are investigated experimentally for the different types of stabilizer. Finally, the analytical and experimental results are compared.

• Steel and Composite Structures
• /
• 제45권3호
• /
• pp.349-367
• /
• 2022

In this research, an approach combining a semi-analytical method and an analytical method is presented to investigate the static and dynamic post-buckling behavior of the sandwich functionally graded (FG) porous cylindrical shells exposed to external pressure. The sandwich cylindrical shell considered is composed of a viscoelastic core and two FG porous (FGP) face layers. The viscoelastic core is made of Kelvin-Voigt-type material. The material properties of the FG porous face layer are considered continuous through each face thickness according to a porosity coefficient and a volume fraction index. Two types of sandwich FG porous viscoelastic cylindrical shells named Type A and Type B are considered in the research. Type A shell has the porosity evenly distributed across the thickness direction, and Type B has the porosity unevenly distributes across the thickness direction. The FG face layers are considered in two cases: outside metal surface, inside ceramic surface (OMS-ICS), and inside metal surface, outside ceramic surface (IMS-OCS). According to Donnell shell theory, von-Karman equation, and Galerkin's method, a discretized nonlinear governing equation is derived for analyzing the behavior of the shells. The explicit expressions for static and dynamic critical buckling loading are thus developed. To study the dynamic buckling of the shells, the governing equation is examined via a numerical approach implementing the fourth-order Runge-Kutta method. With a procedure presented by Budiansky-Roth, the critical load for dynamic post-buckling is obtained. The effects of various parameters, such as material and geometrical parameters, on the post-buckling behaviors are investigated.