• 제목/요약/키워드: Force simulation

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CAE를 이용한 파워트레인의 가진력 해석 (Excitation Force Analysis of a Powertrain Based on CAE Technology)

  • 김성종;이상권
    • 한국정밀공학회지
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    • 제25권12호
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    • pp.107-116
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    • 2008
  • The excitation force of a powertrain is one of major sources for the interior noise of a vehicle. This paper presents a novel approach to predict the interior noise caused by the vibration of the power rain by using the hybrid TPA (transfer path analysis) method. Although the traditional transfer path analysis (TPA) is useful for the identification of powertrain noise sources, it is difficult to modify the structure of a powertrain by using the experimental method for the reduction of vibration and noise. In order to solve this problem, the vibration of the power rain in a vehicle is numerically analyzed by using the finite element method (FEM). The vibration of the other parts in a vehicle is investigated by using the experimental method based on vibrato-acoustic transfer function (VATF) analysis. These two methods are combined for the prediction of interior noise caused by a power rain. Throughout this research, two papers are presented. This paper presents a simulation of the excitation force of the power rain exciting the vehicle body based on numerical simulation. The other paper presents a prediction of interior noise based on the hybrid TPA, which uses the VATF of the car body and the excitation force predicted in this paper.

전차선과 팬터그래프 사이의 동적 상호작용 시뮬레이션 (Simulation of the Dynamic Interactions between Catenary and Pantograph)

  • 권삼영;김길상
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1995년도 하계학술대회 논문집 A
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    • pp.455-459
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    • 1995
  • Catenary/pantograph system consists of overhead lines which have non-uniform elasticity and pantographs which move at high speed and give force to the lines, therefore happen to be failed in contacts between both from time to time. In this study, as the first step to develop a dynamic simulation program, the general theory is discussed for catenary/pantograph system and appropriate modelling. And comparison is conducted with the references after making a program which referred to the contact force equation algorithm. On this algorithm, the unknown contact force is computed by the equations which was induced as combining catenary and pantograph motion equations expressed in finite difference form. Another simulation program based on the assumed contact forces algorithm was developed. In this algorithm, numerical integraion of both the overhead line and pantograph equations, which without combining, are effected for two assumed values of contact force. The correct contact force is then obtained from these two sets of results by linear interpolation to satisfy the contact condition. Through the comparative review on the outputs from this program, it is verified that this algorithm is reliable.

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SW Program Development of a Real-Time Flight Data Acquisition and Analysis System for EO/IR Pod

  • Kim, Songhyon;Cho, Donghyurn;Lee, Sanghyun;Kim, Jongbum;Choi, Taekyu;Lee, Seungha
    • 항공우주시스템공학회지
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    • 제15권6호
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    • pp.42-49
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    • 2021
  • To develop a high-resolution electro-optical/infrared (EO/IR) payload to be mounted on a high-speed and performance fighter aircraft in an external POD for acquiring daytime and nighttime image information on tactical targets, simulations, including flight environments and maneuvers, should be performed. Such simulations are pertinent to predicting the performance of several variables, such as aerodynamic force and inertia load acting on the payload. This paper describes the development of a flight data acquisition and analysis system based on flight simulation software (SW) for mission simulation of super-maneuverability fighter equipped with EO/IR payload. The effectiveness of the system is verified through comparison with actual flight data. The proposed flight data acquisition and analysis system based on FlightGear can be used as an M&S tool for system performance analysis in the development of the EO/IR payload.

Numerical simulation of propeller exciting force induced by milling-shape ice

  • Wang, C.;Li, X.;Chang, X.;Xiong, W.P.
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제11권1호
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    • pp.294-306
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    • 2019
  • On the basis of the Computational Fluid Dynamics technique (CFD) combined with the overlap grid method, this paper establishes a numerical simulation method to study the problem of ice-propeller interaction in viscous flow and carries out a simulation forecast of the hydrodynamic performance of an ice-class propeller and flow characteristics when in the proximity of milling-shape ice (i.e., an ice block with a groove cut by a high-speed revolving propeller). We use a trimmed mesh in the entire calculation domain and use the overlap grid method to transfer information between the domains of propeller rotation calculation and ice-surface computing. The grid is refined in the narrow gap between the ice and propeller to ensure the accuracy of the flow field. Comparison with the results of the experiment reveals that the error of the hydrodynamic performance is within 5%. This confirms the feasibility of the calculation method. In this paper, we calculate the exciting force of the propeller, analyze the time domain of the exciting force, and obtain the curve of the frequency domain using a Fourier transform of the time-domain curve of the exciting force. The existence of milling-shape ice before the propeller can greatly disturb the wake flow field. Unlike in open water, the propeller bearing capacity shows a downward trend in three stages, and fluctuating pressure is more disordered near the ice.

워게임 시뮬레이션에서 전장상황을 고려한 최적경로 모델링 및 시뮬레이션 (Modeling and Simulation of Optimal Path Considering Battlefield-situation in the War-game Simulation)

  • 이성용;장성호;이종식
    • 한국시뮬레이션학회논문지
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    • 제19권3호
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    • pp.27-35
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    • 2010
  • C4I체계를 활용한 워게임은 부대의 전투력과 지휘관의 지휘판단능력을 향상시키고 있다. 워게임 시뮬레이션 과정에서 부대의 기동을 위해 부대 이동계획을 수립하고 있으며, 지휘관이 이동 계획에 따라 작전명령을 하달한다. 만약 워게임 훈련에서 대항군의 포병공격으로부터 아군의 피해를 최소화하고, 대항군에 대한 공격과 방어에 유리한 지역을 우선적으로 점령하면 전장에서 우위를 이끌어 갈 수 있다. 본 논문에서는 전장지역에서 발생하는 상황을 고려하여 소부대가 안전하고 신속하게 이동할 수 있는 최적 경로를 유전자 알고리즘을 통해 생성하고, 유전자 알고리즘을 통해 소부대 최적 경로 생성 과정을 DEVS 모델링 및 시뮬레이션기법을 이용하여 확인하고자 한다.

고속 식부 기구 설계를 위한 컴퓨터 시뮬레이션 프로그램 개발(II) -힘 분석- (Developement of A Computer Simulation Program for the Design of High Speed Transplanting Mechanism(II) -Force Analysis-)

  • 박홍제;김경욱
    • Journal of Biosystems Engineering
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    • 제18권3호
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    • pp.230-238
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    • 1993
  • The parte(I) of this paper deals with the motion analysis of a gear type high speed planting mechanism of rice transplanters. Following that this part(II) contains force analysis of the mechanism. Forces and moments acting on the mechanism were determined analytically and computer coded for the simulation of them on any IBM PC compatiable machines. The simulation program developed in this study can be used as a design tool and also for a sensitivity analysis.

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드로우비드 전문모델에 관한 연구 (Study on the Drawbead Expert Models)

  • 김준환
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2000년도 춘계학술대회논문집
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    • pp.26-29
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    • 2000
  • drawbead expert models are developed for calculating drawbead restraining force and drawbead-exit thinnings which are boundary conditions in FEM stamping simulation employing the linear multiple regression method by which the deviation of drawing characteristics between drawing test and mathematical model is minimized. In order to show the efficiency and accuracy of an expert drawbead model a finite element simulation of auto-body panel stamping is carried out. The finite element simulation shows that the expert drawbead model provides the accurate solution guarantees the stable convergence and the merit in the computation time.

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S-K 구성방정식을 이용한 프린터용 3D Ti-6Al-4V 재료의 유동응력 결정 및 절삭력 예측 (Determination of Flow Stress and Cutting Force Prediction of Ti-6Al-4V Material for 3D Printer using S-K Constitutive Equation)

  • 박대균;김태호;전언찬
    • 한국기계가공학회지
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    • 제17권6호
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    • pp.68-74
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    • 2018
  • Study on the Ti-6Al-4V have been carried out using cutting simulation, and researches for cutting force and chip shape prediction have been actively conducted under various conditions. However, a 3D printer application method using Ti-6Al-4V metal powder material as a high-power method has been studied for the purpose of prototyping, mold modification and product modification while lowering material removal rate. However, in the case of products / parts made of 3D printers using powder materials, problems may occur in the contact surface during tolerance management and assembly due to the degradation of the surface quality. As a result, even if a 3D printer is applied, post-processing through cutting is essential for surface quality improvement and tolerance management. In the cutting simulation, the cutting force and the chip shape were predicted based on the Johnson-Cook composition equation, but the shape of the shear type chip was not predictable. To solve this problem, we added a damaging term or strain softening term to the Johnson-Cook constitutive equation to predict chip shape. In this thesis, we applied the constant value of the S-K equations to the cutting simulation to predict the cutting force and compare with the experimental data to verify the validity of the cutting simulation and analyzed the machining characterization by considering conditions.

Thermal wetting 현상이 탄소나노튜브-금속박막 계면의 응착력에 미치는 영향에 관한 분자 시뮬레이션 연구 (A Molecular Simulation on the Adhesion Control of Metal Thin Film-Carbon Nanotube Interface based on Thermal Wetting)

  • 이상훈;김현준
    • Tribology and Lubricants
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    • 제39권1호
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    • pp.8-12
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    • 2023
  • This study presents a molecular simulation of adhesion control between carbon nanotube (CNT) and Ag thin film deposited on silicon substrate. Rough and flat Ag thin film models were prepared to investigate the effect of surface roughness on adhesion force. Heat treatment was applied to the models to modify the adhesion characteristics of the Ag/CNT interface based on thermal wetting. Simulation results showed that the heat treatment altered the Ag thin film morphology by thermal wetting, causing an increase in contact area of Ag/CNT interface and the adhesion force for both the flat and rough models changed. Despite the increase in contact area, the adhesion force of flat Ag/CNT interface decreased after the heat treatment because of plastic deformation of the Ag thin film. The result suggests that internal stress of the CNT induced by the substrate deformation contributes in reduction of adhesion. Contrarily, heat treatment to the rough model increases adhesion force because of the expanded contact area. The contact area is speculated to be more influential to the adhesion force rather than the internal stress of the CNT on the rough Ag thin film, because the CNT on the rough model contains internal stress regardless of the heat treatment. Therefore, as demonstrated by simulation results, the heat treatment can prevent delamination or wear of CNT coating on a rough metallic substrate by thermal wetting phenomena.

구속받는 3차원 유연 매니퓨레이터의 진동억제 제어 (Vibration Suppression Control of Constrained Spatial Flexible Manipulators)

  • 김진수;우찌야마마사루
    • 한국정밀공학회지
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    • 제17권7호
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    • pp.189-195
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    • 2000
  • For free motions, vibration suppression of flexible manipulators has been one of the hottest research topics. However, for constrained motions, a little effort has been devoted for vibration suppression control. Using the dependency of elastic deflections of links on contact force under static conditions, vibrations for constrained planar two-link flexible manipulators have been suppressed successfully by controlling the contact force. However, for constrained spatial multi-link flexible manipulators, the vibrations cannot be suppressed by only controlling the contact force. So, the aim of this paper is to clarify the vibration mechanism of a constrained, multi-DOF, flexible manipulator and to devise the suppression method. We apply a concise hybrid position/force control scheme to control a flexible manipulator modeled by lumped-parameter modeling method. Finally, a comparison between simulation and experimental results is presented to show the performance of our method.

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