• Journal of Energy Engineering
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• v.10 no.4
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• pp.335-341
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• 2001

Pressure pulsations generated by the blade-tongue interaction induce vibration of the piping systems and the structure connected to pumps, resulting in the severe noise and fatigue fracture. Experiments were made on the natural frequencies of liquid columns in piping systems with a single suction, single stage, centrifugal volute pump. Experimental results show that the natural frequencies of the liquid columns in the pump piping systems depend on the dimensions of the pipes and the impeller shapes, and are not affected substantially by the rate of discharge and the rotating speed of the pump.

• 한국전산유체공학회:학술대회논문집
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• 2010.05a
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• pp.131-135
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• 2010

In the present study, the effects of the stagger angles on the aerodynamic performances in the vaned centrifugal compressor has been investigated by CFD methods. The diffuser vane angles were vane angles were varied in the range of ${\pm}10$ deg. from the intial-design points. The commercial Navier-Stokes solver, ANSYS-CFX were applied to solve the impeller-diffuser flowfields. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.

• Journal of computational fluids engineering
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• v.15 no.3
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• pp.60-65
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• 2010

In the present study, the effects of the stagger angles on the aerodynamic performances in the vaned centrifugal compressor has been investigated by CFD methods. The diffuser vane angles were varied in the range of ${\pm}10$ deg. from the initial-design points. The commercial Navier-Stokes solver, ANSYS-CFX were applied to solve the impeller-diffuser flowfields. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.

• Monthly Korean Chicken
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• s.133
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• pp.124-128
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• 2006

최근 계사 내 바닥관리의 중요성과 더불어 자리깃의 관리가 중요시되고 있다. 소비자의 계육에 대한 까다로운 품질의 요구가 증가되고 있고, 2007년 개체 포장 실시에 따라 유통의 변화에 따라 닭고기의 품질이 더욱 중요시되고 있기 때문이다. 따라서 품질 좋은 닭고기 생산을 위해서는 사육 환경 개선이 필수적인데, 현재 우리나라 계사들의 노후화가 빠르게 진행되고 있다. 일부 농가들이 선도로 시설 재투자 및 닙플 급수기, 단열 및 환기 등 계사 환경개선을 획기적으로 리모델링하여 여러 농가에 희망을 주고 있으며 이런 붐을 타고 많은 농가가 개선을 서둘고 있는 상황이어서 다행한 일이라고 볼 수 있다. 하지만, 이제는 계열사가 주도하여 농가에 지속적인 투자를 독려하고 시설에 대한 개선을 해야 한다고 판단된다. 최근 닭고기 품질과 관련하여 각 계열사는 그 동안 사각지대였던 사육의 환경개선에서 그 해법을 찾고자 노력하고 있지만, 주변 환경과 농가들과의 수익 변수 때문에 항상 평행선을 달려 왔다. 그러나 이제는 성숙한 대화와 조심스런 개선책을 함께 공유해야 할 것이다.

• Journal of computational fluids engineering
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• v.16 no.3
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• pp.75-81
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• 2011

The turbo blowers having large power capacity are generally composed of the variable inlet guide vane, the impeller and the variable diffuser. In the present study, the effect of the stagger angles on the aerodynamic performances has been investigated by CFD methods. The design specifications of the reference model having 400kW power were given as 7.43kg/s of mass flow rate, 1.66 of pressure ratio with 12000rpm of impeller rotating speed. As the first simulation parameter, the diffuser vane angle was varied in the range of ${\pm}$20 degree from the initial-design point. The inlet guide vane angles, as the second one, was changed in the range of ${\pm}$40 degree from the initial-design point. The commercial Navier-Stokes solver, ANSYS-CFX, was applied to solve the three-dimensional unsteady flow fields inside the turbo blower. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.10a
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• pp.20-20
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• 1999

고대로부터 이용되어온 풍력에너지는 특히 풍황이 양호한 서유럽을 중심으로 꾸준히 개발되어 왔다. 최근 세계 여러 나라에서는 화석에너지의 고갈과 심각한 환경오염 문제 등으로 인하여 청정에너지의 개발에 많은 투자를 하고있으며 이에 따라 우리 나라에서도 풍력발전기의 개발이 진행되고 있다. 풍력에너지의 효율적인 이용을 위해서 여러 가지 형태의 발전시스템이 시도되어 왔으나 최근에는 성능 및 효율성이 우수하고 일정 출력을 낼 수 있도록 깃 각 조정이 가능한 수평축 풍력발전시스템이 주로 사용되고 있으며 대형화함으로서 대두되는 경량화 문제를 해결하기 위해 복합재를 이용한 회전날개를 개발하여 이를 사용하고 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.15-15
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• 2000

두 개의 사각형 유입구가 $90^{\cire}$의 각도를 이루고 있는 액체 램제트 엔진의 연소실 형상을 최적화하기 위해서 수조를 이용한 연소실 유동 계측 실험을 수행하였다. 공기 유입구의 연소실 유입 각도는 $30^{\cire}$, $45^{\cire}$ 및 $60^{\cire}$인 세 가지 형상의 연소실 모형을 제작하였으며, 각각의 유입 각도에 대하여 연소실 재순환 영역의 크기를 5가지로 변화시킬 수 있도록 모형을 제작하였다. 그리고 연소실의 배면은 돔의 형태로 하여 재순환이 잘 이루어지도록 모형을 제작하였으며, 유입구에서 연소실로 들어가는 유동의 안정화를 위해 안내깃을 세 개 설치하여 실험하였다.(중략)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.1
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• pp.12-21
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• 2010

This paper focuses on the hover performance experiment of a small-scale single rotor in partial ground conditions. In this study, small-scale rotor blade rotating device and floor panel are used to include partial ground effect. Thrust and torque were measured with varying collective pitch angles at fixed rotor rotating speed. The overlap distance between rotor and ground is d, the rotor diameter is D. It was shown that the ground effects have little effect on the rotor performance until d/D is 0.25. Four blade rotor has more increased thrust and more reduced power than those of two blade rotor because of stronger ground effect. In addition, it was also found that the thrust increases as a collective pitch angle become smaller. Based on these experiment results, we deduced new empirical equation considered blade number and partial ground effect.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.5
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• pp.513-520
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• 2014

An unmanned aerial vehicle (UAV) should be designed to be as small and lightweight as possible to optimize the efficiency of changing the blade shape to enhance the aerodynamic performance, such as the thrust and power. In this study, a computational fluid dynamics (CFD) simulation of an unmanned multi-rotor aerial vehicle in hover mode was performed to explore the thrust performance in terms of the blade rotational speed and blade shape parameters (i.e., taper ratio and twist angle). The commercial ADINA-CFD program was used to generate the CFD data, and the results were compared with those obtained from blade element theory (BET). The results showed that changes in the blade shape clearly affect the aerodynamic thrust of a UAV rotor blade.

• Transactions of the Korean Society of Automotive Engineers
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• v.5 no.5
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• pp.197-212
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• 1997

The performance of a torque converter can be expressed by the performance parameters such as flow radius and flow angle, on the mean flow path. The geometric analysis of the torque converter is required to determine these parameters for the modeling of the torque converter. In general, the blade shape is depicted by three dimensional data at the mid-surface of blade or those of the pressure and suction side. To generate three dimensional model of the blade using the data mentioned above, a consistent data format and a shape generation algorithm are required. This paper presents a useful consistent data format of the blades and an algorithm for the geometrical shape generation. By the geometric analysis program to which the shape generation algorithm is embedded, the variation of blade angles in rotating element analyzed. Then finally, the analyzed results of geometric profile of a blade are compared with those of the blade design principle, so called forced vortex theorem.