• Journal of ILASS-Korea
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• v.1 no.4
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• pp.40-45
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• 1996

This Paper addresses to spray characteristics in w-shaped diesel engine combustion chamber which has impingement parts for 4 sprays injected from an injector. The two-dimensional shapes have been chosen to avoid the difficulties for analysing the spray dynamics in the real chamber. The simple shapes are reproduced with same geometries in vertical or horizontal sections through the impingement lands. The spray developments are visualized with a high speed drum camera and shadowgraphy optical system, and the droplet sizes are measured by Malvern system. The detailed discussions m made for the two different combustion chamber shapes, which are new w-shape using spray wall impaction and general w-shape. The results show that the spray characteristics of the new shape are superior to those of the general w-shape.

• Journal of ILASS-Korea
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• v.3 no.3
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• pp.49-59
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• 1998

The vaporization characteristics and spray combustion processes in the high-pressure environment are numerically investigated. This study employ the high-pressure vaporization model together with the state-of-art spray submodels. The present high-pressure vaporization model can account for transient liquid heating, circulation effect inside the droplet forced convection, Stefan flow effect, real gas effect and ambient gas solubility in the liquid droplets. Computations are carried out for the evaporating sprays, the evaporating and burning sprays, and the spray combustion processes of the turbocharged diesel engine. Numerical results indicate that the high-pressure effects are quite crucial for simulating the spray combustion processes including vaporization, spray dynamics, combustion, and pollutant formation.

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.57-60
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• 2012

본 연구에서는 현재 국내외에서 연구 중인 Blended Wing Body(BWB) 항공기의 엔진흡기 유동을 해석하기 위해 익형과 비행조건을 변화시켜 가며 전산유체해석을 수행하였다. 엔진의 위치에 따라 엔진이 효율적으로 동작하기 위한 조건인 흡기에서의 유동 속도와 그 분산을 중심으로 해석한 결과 익형 표면에서는 경계층의 영향으로 엔진흡기에서 유동속도가 낮고, 속도분산이 높음을 확인할 수 있었다. 한편, 익형 아랫면에서는 높은 비행속도에서 속도분산이 급격히 증가하였다. 이를 통해, 해석에 사용한 익형이 BWB의 동체로 활용하기에 적합한 엔진흡기조건을 갖는지 판별하였다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2003.11a
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• pp.78-83
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• 2003

General algorithm is developed for the prediction of internal flow-induced noise. This algorithm is based on the integral formula derived by using the General Green Function, Lighthills acoustic analogy and Curls extension of Lighthills. Novel approach of this algorithm is that the integral formula is so arranged as to predict frequency-domain acoustic signal at any location in a duct by using unsteady flow data in space and time, which can be provided by the Computational Fluid Dynamics Techniques. This semi-analytic model is applied to the prediction of internal aerodynamic noise from a throttle valve in an automotive engine. The predicted noise levels from the throttle valve are compared with actual measurements. This illustrative computation shows that the current method permits generalized predictions of flow noise generated by bluff bodies and turbulence in flow ducts.

• Transactions of the Korean Society of Automotive Engineers
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• v.8 no.5
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• pp.121-128
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• 2000

Simple design methods were developed to control the coolant flow rates through cylinder head gasket holes. Applying the concept of flow through an obstruction the ratio of intake to exhaust side flow rates could be easily controlled while maintaining the flow rates per cylinder of the original model. Flow distribution in the coolant passage of the original model was calculated by CFD and the flow rates at the gasket holes were modified based on the calculation results. The calculated flow rated of the modified gasket holes were reasonably close to target values. For more accurate control of the flow rate distribution, a design method with iterative CFD calculations was also suggested. The final size of gasket holes for the target flow rates were obtained just after a few optimization iterations. These methods can be very useful for the optimization of heat transfer characteristics in engine cylinder head and block.

• Proceedings of the KIEE Conference
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• 1997.07b
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• pp.587-589
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• 1997

In this paper we design the model following ${\mu}$-synthesis control system for optimal fuel-injection of diesel engine using genetic algorithms. To do this, we give gain and dynamics parameters to the weighting functions and apply genetic algorithms with reference model to the optimal determination of weighting functions that are given by D-K iteration method which can design ${\mu}$-synthesis controller in the state space. These weighting functions are optimized simultaneously in the search domain selected adequately. The effectiveness of this ${\mu}$-synthesis control system for fuel-injection is verified by computer simulation.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.739-740
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• 2010

Numerical studies were performed to investigate an effective water cooling type for reducing the thermal load of deflector in test facility with two cooling types and various mass flow rate conditions. According to analyses a core water injection type was superior to a side water injection fro the viewpoint of reducing the thermal load of deflector.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.606-608
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• 2017

The computational fluid analysis was carried out to investigate structural stability of exhaust duct for turboprop engine. In order to calculate the thrust and shear force acting on the flight condition of the aircraft, the flow in the exhaust duct and the flow in the direction of the exhaust duct flange were analyzed by Fluent software to obtain thrust, shear force and bending moment. As a result of the analysis, it was confirmed that the allowable loads set idle engine manual were not exceeded.

• 유체기계공업학회:학술대회논문집
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• 1999.12a
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• pp.141-146
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• 1999

The comming of high speed computers with large memory size in recent years has allowed the practical development of codes which solve the Reynolds-averaged NAvier-Stokes (RANS) equations in three dimensions. Such codes are already used by the large engine manufacturers for the advanced design of some engine components. Different computational fluid dynamics approaches and turbulence models exist, and it seems essential today to establish their degree of validity for application to typical configurations in turbomachinery. In 1993 the Turbomachinery Committee of the IGTI of ASME has issued an open invitation to predict the flow details of an isolated transonic fan rotor called as NASA ROTOR 37. This paper reports this test case.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.239-242
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• 2004

In this paper, the general mathematical model of LRE(Liquid Rocket Engine) is presented. For the analysis about the trend of dynamics and the stability of open type LRE, it is transformed to linear model by Laplace transform and synthesized to the linear complex model of LRE with Matlab/Simulink.