• Title/Summary/Keyword: Simulation Comparison

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Numerical simulation of hypervelocity impacts on laminated composite plate targets using SPH method (SPH 기법을 이용한 복합 적층판의 초고속 충돌 해석)

  • Lee, Jae-Hoon;Seo, Song-Won;Min, Oak-Key
    • Proceedings of the KSME Conference
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    • 2004.11a
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    • pp.331-336
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    • 2004
  • This paper is concerned with numerical simulation of hypervelocity impacts(HVIs) of a projectile on laminated composite plate targets using SPH method. A one-parameter visco-plasticity model and damage model is used to describe the HVIs response of composite materials. The numerical simulation was carried out for a steel projectile striking to aluminum plate targets and for an aluminum projectile striking to laminated graphite/epoxy (Gr/Ep) composite plate targets. Through the numerical simulation, comparison with the HVIs response of isotropic materials and composite materials is discussed.

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DEVELOPMENT OF VEHICLE DYNAMICS MODEL FOR REAL-TIME ELECTRONIC CONTROL UNIT EVALUATION SYSTEM USING KINEMATIC AND COMPLIANCE TEST DATA

  • KIM S. S.;JUNG H. K.;SHIM J. S.;KIM C. W.
    • International Journal of Automotive Technology
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    • v.6 no.6
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    • pp.599-604
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    • 2005
  • A functional suspension model is proposed as a kinematic describing function of the suspension, that represents the relative wheel displacement in polynomial form in terms of the vertical displacement of the wheel center and steering rack displacement. The relative velocity and acceleration of the wheel is represented in terms of first and second derivatives of the kinematic describing function. The system equations of motion for the full vehicle dynamic model are systematically derived by using velocity transformation method of multi-body dynamics. The comparison of test and simulation results demonstrates the validity of the proposed functional suspension modeling method. The model is computationally very efficient to achieve real-time simulation on TMS 320C6711 150 MHz DSP board of HILS (hardware-in-the-loop simulation) system for ECU (electronic control unit) evaluation of semi-active suspension.

Development of a nonlinear biomechanical soft tissue model for a virtual surgery trainer (가상수술기를 위한 비선형 생체 모델의 개발)

  • Kim J.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2005.06a
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    • pp.911-914
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    • 2005
  • Soft tissue characterization and modeling based on living tissues has been investigated in order to provide a more realistic behavior in a virtual reality based surgical simulation. In this paper, we characterize the nonlinear viscoelastic properties of intra-abdominal organs using the data from in vivo animal experiments and inverse FE parameter estimation algorithm. In the assumptions of quasi-linear-viscoelastic theory, we estimated the nonlinear material parameters to provide a physically based simulation of tissue deformations. To calibrate the parameters to the experimental results, we developed a three dimensional FE model to simulate the forces at the indenter and an optimization program that updates new parameters and runs the simulation iteratively. The comparison between simulation and experimental behavior of pig intra abdominal soft tissue are presented to provide a validness of the tissue model using our approach.

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Comparison of parameter estimation methods for normal inverse Gaussian distribution

  • Yoon, Jeongyoen;Kim, Jiyeon;Song, Seongjoo
    • Communications for Statistical Applications and Methods
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    • v.27 no.1
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    • pp.97-108
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    • 2020
  • This paper compares several methods for estimating parameters of normal inverse Gaussian distribution. Ordinary maximum likelihood estimation and the method of moment estimation often do not work properly due to restrictions on parameters. We examine the performance of adjusted estimation methods along with the ordinary maximum likelihood estimation and the method of moment estimation by simulation and real data application. We also see the effect of the initial value in estimation methods. The simulation results show that the ordinary maximum likelihood estimator is significantly affected by the initial value; in addition, the adjusted estimators have smaller root mean square error than ordinary estimators as well as less impact on the initial value. With real datasets, we obtain similar results to what we see in simulation studies. Based on the results of simulation and real data application, we suggest using adjusted maximum likelihood estimates with adjusted method of moment estimates as initial values to estimate the parameters of normal inverse Gaussian distribution.

Random Vibration of Non-linear System with Multiple Degrees of Freedom (다자유도 비선형계의 불규칙 진동 해석)

  • Lee, Sin-Young
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.15 no.5
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    • pp.21-28
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    • 2006
  • Vibration of a non-linear system with multiple degrees of freedom under random parametric excitations was evaluated by probabilistic method. The non-linear characteristic terms of system structure were quasi-linearized and excitation terms were remained as they were. An analytical method where the expectation values of square mean of error was minimized was used. The numerical results were compared with those obtained by Monte Carlo simulation. A linear congruential generator and Box-Muller method were used in Monte Carlo simulation. The comparison showed the results by probabilistic method agreed well with those by Monte Carlo simulation.

A Study on the WECPNL Application Method to Estimate the Measured data by using the Simulated value for Military Aircraft (군용항공기의 예측 최고소음도와 측정된 최고소음도의 비교를 통한 WECPNL의 산정에 관한 연구)

  • Kim, Bong-Suk;Chang, Seo-Il;Lee, Yeon-Soo
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2007.05a
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    • pp.604-608
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    • 2007
  • The INM simulation program is used to estimate the condition of the exposed area to the noise near a military airport in Korea. $WECPNL_k$, the evaluation unit of korean airport noise, is different from the ICAO $WECPNL_I$ that is used in the simulation program. Therefore, it is inappropriate to compare these units each other directly. This study presents method of comparison between them by using $LA_{MAX}$. The aircraft events are classified into three classes, as departure, overfly and approach. In result, the measurement and simulation seemed to be similar at departure and approach pattern. However, overfly pattern had higher errors between measurement and simulation. Finally, it is necessary to examine the method to determine flight events and duration for the $WECPNL_k$ application.

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EFFECTS OF VARIOUS VVA SYSTEMS ON THE ENGINE FUEL ECONOMY AND OPTIMIZATION OF A CVVT-VVL SI ENGINE USING 1D SIMULATION

  • Lee, H.B.;Kwon, H.;Min, K.
    • International Journal of Automotive Technology
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    • v.8 no.6
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    • pp.675-685
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    • 2007
  • A single cylinder SI engine with a VVA system is modeled by the coupling of a commercial 1D simulation package and an additional combustion model and validated by comparison with experimental data. A number of simulations are carried out to investigate the effects of five different VVA systems on the performance and fuel efficiency of the baseline engine. Finally, the simulation model is applied to an extensive computational study to map out the strategies to operate the engines with dual CVVT and dual CVVT-2 step VVL systems in a fuel-efficient manner.

A Study on the Comparison of Calculated the Indoor Illuminance Values by Lighting Simulation Softwares for Suitable Prediction About Indraft of Daylight (자연채광 유입에 따른 실내 조도의 적합한 예측을 위한 조명시뮬레이션 소프트웨어 비교 연구)

  • Kim, Yu-Sin;Choi, An-Seop
    • Proceedings of the Korean Institute of IIIuminating and Electrical Installation Engineers Conference
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    • 2007.05a
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    • pp.92-96
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    • 2007
  • Architecture design has need of daylight prediction to utilize daylight efficiently. But it is difficult to predict the exact value of available daylight in buildings. Using various lighting simulation software is not difficulty, but we can find different results under the same conditions. The purpose of this paper is to compare simulation values from various software such as Lumen-micro 2000, Lightscape 3.2, and Relux 2006. The same space and parameters of daylight(location of space and window, date, time, and skylight condition) are considered to conduct various simulation conditions.

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A COMPARISON STUDY OF WIND TUNNEL TEST AND AERODYNAMIC ANALYSIS FOR TARGET DRONE (무인비행체 풍동시험과 공력해석의 비교 연구)

  • Kim, H.I.;Kim, J.S.;Lee, S.M.;Kim, K.T.;Kim, M.K.
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.17-20
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    • 2010
  • An aerial target system is used for the purpose of experimental test and fire training of missile that newly developed and in mass production. Since the target drones of aerial target systems are monopolized by several major countries so that they are selling at a high price. In this paper, we present the CFD simulation results on a new target drone that Kyungan co. ltd is developing with their own technologies. The presented CFD simulation was conducted in the same conditions of a wind tunnel tests and we could obtain the simulation results of the lift and drag values were in errors by less than 15 percent compared to the experiment. The simulation results were used to determine the modified shapes of new prototype target drone that could fly safely.

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Simulation of Operation Performance for DG Prime Mover (디젤발전기 원동기의 운전특성 시뮬레이션)

  • 최순만;오진석
    • Journal of Advanced Marine Engineering and Technology
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    • v.21 no.2
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    • pp.166-177
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    • 1997
  • The prime mover performance of on - board Diesel Generator is well characterized by the variation of frequency and the load sharing on parallel running under electric load change. This study is aimed to configure the modeling for performance simulation regarding to DG operation which could be interested for education purpose or system analysis. The modeling had been made on the base of modules such as govenor, prime mover of diesel engine and generator with electric load system, which were then intergrated for total simula¬tion performance. One real model system has been introduced for deciding relating parameters and for the comparison of resulting performance in simulation. The responses from the modelling were confirmed in single and paralell operation, the results of which showed resonable accordance with the real system.

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