• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2000년도 춘계학술대회논문집B
• /
• pp.765-770
• /
• 2000

Hot-wire measurements are reported on the developing turbulent flows subject to plane rate of strain in a rotating $90^{\circ}$ dog bend. The cross-section of the bend varies from $100mm{\times}50mm$ rectangular shape at the bend inlet gradually to the $50mm{\times}100mm$ shape at the bend outlet with remaining a constant area. Data signals from the rotating test section are transmitted through a slip ring to the personal computer which is located at the outside of the rotating disc. 3-dimensional velocity and 6 Reynolds stress components were calculated from the equations which correlate the fluctuating and mean voltage values measured with rotating a slant type hot-wire into 6 orientations. The effects of Coriolis and centrifugal forces on the mean motions and turbulence structures are investigated with respect to rotational speed.

• 한국진공학회지
• /
• 제12권2호
• /
• pp.79-85
• /
• 2003

다단 원판형 드래그펌프의 배기특성을 출구측 압력변화에 따른 입구측의 압력을 측정함으로써 파악하였다. 압력측정범위는 유량이 없을 때 출구측에서 0.13∼533 Pa로 하였다. 펌프 로터의 회전 속도는 24,000rpm이며, 질소가스를 사용하여 유량에 대한 성능실험을 수행하였다. 본 연구에서는 원판의 단의 수에 따른 원판형 드래그 펌프의 성능을 측정하였다. 3단, 2단, 단단형으로 원판형 드래그펌프를 구성하여 성능 실험하였으며, 최대도달진공도, 최대압축비, 배기속도등을 각각 측정하여 상호 성능을 비교·고찰하였다.

• 대한조선학회논문집
• /
• 제30권1호
• /
• pp.30-44
• /
• 1993

추진 효율 향상을 위한 비대칭형 전류 고정날개-프로펠러 추진 시스템의 성능해석에 대한 이론적 실험적 고찰과 이에 대한 비교를 수행하였다. 성능해석을 위한 비대칭 및 대칭 해석 프로그램은 양력면 이론에 의해 개발되어졌으며, 실험과의 상호관계를 통하여 보다 정도 높은 설계 및 성능해석을 수행할 수 있도록 만들어졌으며 특히 불균일 반류에서의 고정날개 성능해석을 통한 비대칭 설계가 가능하여 졌다. 개발된 프로그램을 이용하여 새로운 비대칭 고정날개를 설계하였으며 성능해석을 이론적으로 수행한 결과 단독 프로펠러에 비하여 약 6%의 효율증가를 보이고 있다.

• Journal of Ship and Ocean Technology
• /
• 제6권1호
• /
• pp.27-33
• /
• 2002

Recently, the application of the electric propulsion system becomes popular because of its advantage over conventional propulsion. However, the complicated flow mechanism and interaction around the azimuth thruster are not fully understood yet, and the studies on the powering performance characteristics with azimuth/pod thrusters are now in progress. The experimental method developed in KRISO(Korea Research Institute of Ships & Ocean Engineering) is introduced and the results of the powering performance tests, consisting of resistance, self-propulsion and propeller open water tests for a cable layer with two azimuth thrusters are presented. For the analysis of powering performance with azimuth thrusters, it is necessary to evaluate the thrust/drag for components of a thruster unit, Extrapolation results could differ according to the various definitions of the propulsion unit; that is the pod, thruster leg and/or nozzle can be treated as hull appendages or as part of propulsion unit, The powering performances based on several definitions are investigated for this vessel. The results of the measurements for the 3-dimensional velocity distribution on the propeller plane are presented to understand the basis of the difference in propulsion characteristics due to the propeller rotational directions.

• 한국인쇄학회지
• /
• 제23권2호
• /
• pp.1-14
• /
• 2005

Generally, printing inks are composed of pigment, vehicle and additive. Among others, the vehicle transfers the pigment to substrate and then binds it on the surface. So, rheological properties of the vehicle are an important factor which has influence on printability. Thus, in this study, rheology of the vehicle was investigated by using rotational rheometer according to molecular weight of resin. Also, emlusion rheology of water in oil type and its microstructure were examined with increasing the shear rate. Consequently, the following results were obtained: (1) By viscometric flow test, zero shear viscosity and shear thinning index of vehicle increased with increasing the molecular weight of resin. (2) By relaxation and creep test, relaxation time and retardation time of vehicle increased with increasing the molecular weight of resin. (3) By frequency sweep test, crossover point of vehicle increased with increasing the molecular weight of resin. (4) G' and G" of emlusions increased with increasing the molecular weight by amplitude sweep test. (5) The shape of water drop in emlusions was changed to the capillary tube.

• 한국유체기계학회 논문집
• /
• 제10권6호
• /
• pp.38-43
• /
• 2007

Pumps for a turbopump generally operate under high rotational speeds and large head rise conditions. Therefore, reliability is a prime design requirement. Floating-ring type seals are frequently employed in a turbopump because of robustness despite of low hydraulic efficiency. There are many researches on the floating-ring seal itself, but the effects of the floating ring seals on the performance of the whole pump are not widely studied in spite of their importance. In the present study, experimental and computational studies on the effects of the radial clearance of the floating ring seals on the performance of a pump were performed. The experimental results showed that the head rise and efficiency increased as the floating-ring seal clearance was decreased. The results also showed the possibility that the leakage flow which was injected to the inlet of the inducer could enhance the suction performance of the inducer by diminishing the size of the backflows.

• 한국유체기계학회 논문집
• /
• 제20권2호
• /
• pp.75-81
• /
• 2017

This paper presents a numerical investigation on the local hydraulic cavitation phenomena of water resulting from the rotor with high rotational speed in the hydraulic cavitation heat generator. The numerical simulation utilizes the standard k-epsilon turbulence model, the mixture multiphase model and the Schnerr-Sauer cavitation model to simulate the complex cavitation phenomena in the generator. For exploring the efficient shape of the dimples on the rotor to causing cavitation phenomena artificially, the pressure distributions and the volume fractions of the vapor on the rotor are investigated respectively about different shapes of the rotor in the generator. The optimum shape of the dimple to causing cavitation phenomena in the selected shapes is obtained by the means of the numerical simulation.

• 한국추진공학회지
• /
• 제8권4호
• /
• pp.76-83
• /
• 2004

CRW Tyre UAV 추진시스템은 수직으로 이착륙이 가능하고 고정익으로 고속 전진 비행이 가능한 개념으로 설계되었다. 이를 위해 추진시스템은 이착륙 시에는 로터를 구동시켜 수직으로 비행하고 고속 비행 시에는 로터를 정지시켜 날개로 사용하고 가스발생기에서 생성된 가스를 주 노즐로 분사하여 본래의 제트엔진으로 사용한다. ICV방법과 SIMULINK를 이용하여 천이 성능 해석을 수행하였다. 연료유량은 터빈 입구온도의 스텝과 과온 현상을 피하기 위해 램프 증가를 하였고 이에 따른 추력의 변화와 터빈 입구온도의 변화를 살펴보았다.

• 대한기계학회논문집
• /
• 제13권3호
• /
• pp.373-384
• /
• 1989

본 논문에서는 상기와 같은 문제들을 규명하기 위하여 비교적 긴 원통에 액체를 내장할 수 있도록 회전체를 제작하여 액체의 종류, 점도, 액체의 양 등을 파라미터로 하여 불안정영역의 범위와 진동진폭에 관해서 실험적으로 조사하였고, 비중이 다른 2액체를 동시에 내장한 경우 액체의 자유표면과 경계면에 의한 진동특성을 을 검토하였다.

• 한국유체기계학회 논문집
• /
• 제18권2호
• /
• pp.67-72
• /
• 2015

The purpose of this study is to achieve energy saving effect of inverter driving multistage centrifugal pump. For determining the operation points in the pump system, the system curves should be obtained experimentally. To get the system curves, three pumps combined in parallel and one pump operated with different rotational speeds. But for variable speed pump system, energy saving rates can not be evaluated from operation efficiencies. That is why operation efficiencies, system curves, duty cycles, and input powers of the pump system were measured by the constructed experimental apparatus. The duty cycle segmented into different flow rates and weighting the average value for each segment by the interval time. The system was operated with two different periods. The mean duty cycles were collected from apartment and found that the system operated at 40% and at 50% or below capacity. Measured energy saving rate was 58.16%. Estimating method of energy saving rate could be more effective operation index than that of operation efficiency.