• 한국분무공학회지
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• 제19권2호
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• pp.64-68
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• 2014

A driving vehicle performance which is driven by FTP-75 mode was simulated by computer. Throttle valve position, engine speed, air mass flow rate, fuel consumption et al. were computer simulated. A set of engine part load performance data, automatic transmission shift map and vehicle specifications were used for the computer simulation. Throttle valve position, engine speed, air mass flow rate et al. measured for evaluating the computer simulation results by driving the vehicle with FTP-75 mode on a chassis dynamometer. GT-Power$^{(R)}$ software was used for the computer simulation of the driving vehicle performance. Experimental fuel consumption rate was measured by using an ECU HILS fuel injection system. The experimental data and simulation results were compared. The computer simulation of the driving vehicle performance predicts the measured data well comparatively.

• 항공우주시스템공학회지
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• 제13권1호
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• pp.38-46
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• 2019

가스터빈 엔진에 대한 엔진 진단기술에 대한 관심이 높아지고 있으며, 엔진 건전성 진단기술에 적용 가능한 정확한 엔진 성능모사 프로그램의 중요성은 점점 더 커지고 있다. 이를 위한 엔진 성능모사는 설계점 해석으로부터 시작하여 탈설계점 성능모사, 부분부하 성능모사를 정확하게 수행해야 할 필요가 있다. 이에 따라 본 연구에서는 2-스풀 분리 배기 방식 터보팬 엔진에 대한 엔진 시뮬레이션 프로그램을 개발하고 PW(Pratt & Whitney)사의 JT9D-7R4G 엔진을 해석하였다. 각 비행영역에서의 설계점과 탈설계점에서의 정상상태 성능모사를 수행하고, 최대이륙조건 설계점과 순항상태 설계점의 해석결과의 차이를 비교하였다. 또한 구성품 성능선도 축척법 중 하나인 Reynold's Correction의 효과를 분석하였다. 개발된 프로그램의 결과와 NPSS의 결과를 비교하여 프로그램을 검증하였다.

• The Journal of the Acoustical Society of Korea
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• 제21권1E호
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• pp.42-48
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• 2002

In this paper, a computer simulation method is presented far the dynamic analysis of a hydraulic engine mount system. The hydraulic engine mount system controls the damping characteristics using the viscosity of fluid flow. The complex stiffnesses of the main rubber for the hydraulic engine mount system are computed using a finite element analysis. The equations of motion considering the parameters of the hydraulic engine mount system are derived. To investigate the effects of the hydraulic engine mount system, the computer simulation running over a typical rough road is carried out using a vehicle dynamic model. These results are compared with those of the conventional rubber mount system.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.213-217
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• 2017

액체로켓엔진 고장에서 시동과정이 30% 이상을 차지하며 특히, 우주왕복선 주 엔진(Space Shuttel Main Engine, SSME)은 2%의 밸브위치 오차 또는 0.1초의 시간오차와 같은 작은 변화에도 급격하게 변화하는 매우 민감한 시스템으로 시동과정의 모델링이 중요하다. 하지만, 시동과정에서 비선형 질량 유량과 열전달 특성 때문에 많은 어려움이 발생한다. 본 논문에서는 이를 해결하기 위하여 부분적인 전산유체해석(Computational Fluid Dynamics, CFD) 방법을 사용하였으며 본 논문에서는 구성품의 모델링을 수행하여 정상상태에서 확인을 하였다.

• 에너지공학
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• 제24권3호
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• pp.61-66
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• 2015

Homogeneous charge compression ignition (HCCI) engine combines the combustion characteristics of a compression ignition engine and a spark ignition engine. HCCI engines take advantage of the high compression ratio and heat release rate and thus exhibit high efficiency found in compression ignition engines. In modern research, simulation has be come a powerful tool as it saves time and also economical when compared to experimental study. Engine simulation has been developed to predict the performance of a homogeneous charge compression ignition engine. The effects of compression ratio, cylinder pressure, rate of pressure rise, flame temperature, rate of heat release, and mass fraction burned were simulated. The simulation and analysis show several meaningful results. The objective of the present study is to develop a combustion characteristics model for a homogeneous charge compression ignition engine running with isooctane as a fuel and effect of compression ratio.

• 한국자동차공학회논문집
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• 제11권4호
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• pp.58-67
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• 2003

An automotive engine cooling system is closely related with overall engine performances, such as reduction of fuel consumption, decrease of air pollution, and increase of engine life. Because of complex reaction between each component, the direct experiment, using a vehicle, takes high cost, long time, and slow response to the system change. Therefore, a computer simulation would provide the designer with an inexpensive and effective tool for design, development, and optimization of the engine cooling system over a wide range of operating conditions. In this work, it has been predicted the thermal performance of the engine cooling system in cases of stationary mode, constant speed mode, and city-drive mode by mathematical modelling of each component and numerical analysis. The components are engine, radiator, heater, thermostat, water pump, and cooling fans. Since the engine model is the most important, that is divided into eight sub-sections. The volume mean temperature of eight sub-sections are simultaneously calculated at a time. For detail calculation, the radiator and heater are also divided into many sub-sections like control volumes in finite difference method. Each sub-section is assumed to consist of three parts, coolant, tube with fin, and air. Hence it has been developed the simulation program that can be used in case of design and system configuration changes. The overall performance results obtained by the program were desirable and the time-traced tendencies of the results agreed fairly well with those of actual situations.

• 한국추진공학회지
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• 제23권4호
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• pp.50-60
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• 2019

본 논문에서는 MATLAB/Simulink를 기반의 우주왕복선 주엔진(Space Shuttle Main Engine, SSME)의 툴박스 개발을 다루었다. 로켓엔진의 수학적 모델링에는 많은 시간과 신뢰성 확보가 필요하다. 로켓엔진 시뮬레이션 툴박스를 개발하면 이를 해결할 수 있으며 업그레이드와 새로운 엔진 개발의 용이성을 기대할 수 있다. SSME의 수학적 모델링은 7개의 지배방정식을 통해 유도한 32개의 미분방정식을 사용하여 구성하였으며 이를 구성요소 별로 모듈을 구별하여 SSME 시뮬레이션 툴박스를 개발하였다. 성능검증을 위하여 기존 시뮬레이션 결과와 비교하여 검증하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제26권2호
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• pp.248-255
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• 2002

Miller cycle was studied and analyzed by engine performance simulation to achieve very low fuel consumption and to meet the IMO NOx regulation on a medium speed diesel engine. Based on the performance simulation results the intake valve closing time for HYUNDAI HiMSEN 6H21/32 engine was set at 0deg.ABDC(After Bottom Dead Center). Also, the simulation results indicated that significant NOx reduction could be achieved with low reduction of fuel consumption. The performance simulation investigated the effect of compression ratio and turbocharger on fuel consumption and NOx concentration in combination with Miller cycle. The results indicated a significant reduction of fuel consumption with keeping NOx concentration. The results of performance simulation were compared with measured data to verify simulation results. The comparison showed the maximum error was 2.34% in exhaust temperature. Also, the experimental result showed that improvement in BSFC(Brake Specific Fuel Consumption) was 5.8g/kwh with keeping NOx level similar to simulation result.

• 한국자동차공학회논문집
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• 제10권5호
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• pp.35-44
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• 2002

Engine cycle simulation using a two-zone model was performed to investigate the effect of the engine parameters on NO and soot emissions in a DI diesel engine. The present model was validated against measurements in terms of cylinder pressure, BMEP, NO emission data with a 2902cc turbocharger/intercooler DI diesel engine. Calculations were made for a wide range of the engine parameters, such as injection timing, ignition delay, Intake air pressure, inlet air temperature, compression ratio, EGR. This parametric study indicated that NO and soot emissions were effectively decreased by increasing intake air pressure, decreasing inlet air temperature and increasing compression ratio. By retarding injection timing, increasing ignition delay and applying EGR. NO emission was effectively reduced, but the soot emission was increased.

• 대한기계학회논문집
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• 제10권3호
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• pp.305-315
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• 1986

본 연구에서는 가변 기통 엔진의 동특성을 규명하기 위해 세곳으로 지지되는 직렬 4기통 디이젤 엔진에 대한 3자유도 모델을 설정하였고, 이 모델에서 각 마운트의 위치와 경사각 및 방진고무의 크기를 변경시킬 때의 최적화 문제를 컴퓨터 시뮬레이션 으로 고찰하였다.