• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2007.11a
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• pp.923-928
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• 2007

The rattle noise originated from the oil-pump system was issued in developing an engine. In this paper, the major concerning factors for rattle noise are analyzed and the NVH developing process is summarized. The main factors are the tip clearance of inner/outer rotor, the clearance between oil pump housing and rotor guide and the rotor mass. Also, the optimization for oil-pump rotor whine noise is performed. The main factors of the rotor whine are the profile of the rotor, the oil pressure and the shape of oil route. This paper will present the design guidelines of the engine oil-pump system.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2006.11a
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• pp.202-207
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• 2006

The aeroacoustic noise from intake head of a vacuum cleaner is caused by complicated transient pressure fluctuation and it greatly affects the overall SPL of the vacuum cleaner. In this study, we intended to decrease the overall SPL by reducing the aeroacoustic noise from intake head. In the first the place, we analyzed the aeroacoustic noise from the unsteady fluid analysis of intake head. And then, we grasped the dominant frequency band from the aeroacoustic noise by comparing the spectrum distributions between examinations and analyses. Also, we systematically investigated the aeroacoustic noise sources from each part composing the intake head. Consequently, we redesigned each part of the dominant noise sources and suggested the modified intake head, resulting in the reduction ortho overall SPL by 3.6dB(A).

• 한국가시화정보학회:학술대회논문집
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• 2005.12a
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• pp.111-116
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• 2005

An automobile engine has the Positive Crankcase Ventilation system (PCV system) for preventing air pollution as the environmental problem is important In this system, a PCV valve is the most important component to control the flow rate of Blowby gas which is generated by various engine powers. But, in the working place, the design of a PCV valve is very difficult because of interaction between fluid and solid motions. In this study, we investigated fluid flow characteristics using re-meshing method of a CFD technique to simulate spool behavior. As the results, a spool is periodically oscillated with time and is largely oscillated in proportion to the differential pressure between inlet and outlet. And, although the velocity at the orifice increases with the differential pressure, the flow rate of the outlet decreases. This research may give PCV designers visual flow information to help them

• Journal of Advanced Marine Engineering and Technology
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• v.17 no.4
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• pp.20-27
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• 1993

Emulsified oily wastewater is generally hard to treat in separating oil and water by conventional separators. In this paper the magnetohydrodynamic water treatment device was used to separate oil from emulsified oily wastewater which contained high conductivity. The emulsified oil removal rates and economic ranges of oil separation at various factors were investigated to confirm the influence of the magnetic field in MHD water treatment device according to the characteristics of emulsion brake. Experimental results proved that the oil removal rates were proportional to Lorentz force which depends on the intensity of magnetic field, conductivity and velocity of wastewater.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2001.05a
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• pp.897-903
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• 2001

The supersonic flutter analysis of cylindrical composite panels subject to thermal stresses has been performed using layerwise nonlinear finite elements. The geometric nonlinear finite elements of cylindrical shells are formulated using hamilton's principle with von Karman strain-displacement relationship. Hans Krumhaar's modified supersonic piston theory is appled to calculate aerodynamic loads for the panel flutter analysis. The present results show that the critical dynamic pressure of cylindrical panels under compressive thermal stresses can be dramatically reduced. The margin of aerothermoelastic stability considering thermal and aerodynamic coupling should be verified in the structural design of launch vehicles and high speed aircrafts.

• Proceedings of the SAREK Conference
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• 2009.06a
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• pp.371-375
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• 2009

The distribution control of refrigerant flow is one of the basic technique to enhance system efficiency. However, if engineers forget to control the refrigerant flow speed in all operation range, refrigerant flow mal distribution becomes a noise source. The refrigerant flow noise should be checked and controlled at the lowest air flow mode which is the most silent mode and frequently used in night time.

• Journal of computational fluids engineering
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• v.4 no.2
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• pp.67-73
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• 1999

In the present paper, three types of the flow solvers were used to investigate the influence on the airfoil shape optimization. The adopted equations, i.e., Euler, thin layer Navier-Stokes and full Navier-Stokes ones. are solved using implicit LU-ADI decomposition scheme. The gradient projection method with the sinusoidal function was used as an optimization algorithm. The present numerical method was applied to the drag minimization problems under the initial shape of NACA0012 airfoils.

• Transactions of The Korea Fluid Power Systems Society
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• v.5 no.1
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• pp.20-26
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• 2008

Various types of hydraulic shock absorbers are widely used in many fields because of its numerous advantages. However, in order to design adequate damping characteristics, accurate flow data near the orifices are required essentially. In this paper, a commercial computational fluid dynamics(CFD) code, FLUENT is adopted to investigate the flow characteristics near orifices of a shock absorber. Static pressure and velocity vector distributions, fluid path lines are presented for compression/tension strokes and various piston speeds. In order to validate the result of analysis, the numerically obtained damping forces are compared with those of analytical estimations obtained by modified Bernoulli equation. The results reported herein will provide better understanding of the detailed flow fields within shock absorber, and the CFD analysis method proposed in this paper can be used in the design of other types of hydraulic shock absorber.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1997.04a
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• pp.608-614
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• 1997

2차원 압축성 오일러 방정식을 지배 방정식으로 하여 음향학적 문제를 직접 수치 계산하였다. Roe의 개략적인 리만해(Approximate Riemann Solver)에 의거하여 대류항을 구성하였고 높은 정확도를 유지하기 위해 Vanleer의 MUSCL 방법을 사용하여 공간을 이산화하였다. 시간 적분으로는 2차의 Runge-Kutta 방법을 사용하였다. Resonance tube 내의 음향학적 문제 해석을 위해 최근까지 제시된 음향 경계 조건들을 비교하였고 각 경계 조건들이 갖는 물리적 의미를 고찰하였다. 이들을 통하여 압력파의 물리적인 행태를 모사하였고 실험과 비교하였다. 계산결과들을 통하여 사용된 방법은 전형적인 압축성 유동 해석 문제 뿐만 아니라 선형, 비선형의 음향학적 문제들을 적절한 경계 조건과 결합하여 해석할 수 있음을 알 수 있었고 resonance tube와 같은 공학적으로 실제적인 문제들에 대한 응용이 기대된다.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1993.11a
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• pp.88-91
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• 1993

유동층 반응기 (H=0.8 m, ID=0.08 m) 에서 폐타이어의 열분해를 수행함에 있어 열분해에 사용되는 열을 외부에서 공급함과 동시에 일부는 내부에서 자체적으로 연소시켜 열을 얻고자 하였다. 온도 증가에 따라 가스의 수율은 40 %까지 증가하였고, 반면에 오일의 수율은 감소하였다. 또한 가스중에 heavy hydrocarbon 이 감소함과 동시에 H$_2$ 및 light hydrocarbon 이 증가하였고 이로 인해 가스 부피당 발열량은 감소하는 것으로 나타났다. 가스의 체류시간도 가스조성에 상당히 영향을 미치는 것으로 나타났으며, 본 시스템에서 발열량 및 가스생성량은 2 u$_{mf}$ 에서 최소치를 나타내는 것으로 보였다. 또한 $O_2$ 농도의 증가는 결국에는 생성가스의 연소를 일으키며, 적당한 $O_2$ 농도의 설정으로 이의 연소를 최소화하는 작업이 필요하다.