• Ocean Systems Engineering
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• 제14권1호
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• pp.53-72
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• 2024

The interaction of the blade of surface-piercing propellers (SPPs) with the water/air surface is a physical phenomenon that is difficult to model mathematically, so that such propellers are usually designed using empirical approaches. In this paper, a newly developed mechanism for measuring the torque of SPPs in an open water circuit is presented. The mechanism includes a single-component load cell and a deformable torque sensor to detect the forces exerted on the propeller. Deformations in the sensor elements lead to changes in the strain gauge resistance, which are converted into voltage using a Wheatstone bridge. The amplified signal is then recorded by a 16-channel data recording system. The mechanism is calibrated using a 6-DoF calibration system and a Box-Behnken design, achieving 99% accuracy through multivariate regression and ANOVA. Finally, the results of performance tests on a 4-blade propeller were presented in the form of changes in the torque coefficient as a function of feed rate. The results show that the new mechanism is 8% more accurate than conventional empirical methods.

• 한국자동차공학회논문집
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• 제16권2호
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• pp.58-65
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• 2008

The finite element programs have been developed for structure, collision, flow, dynamics, heat transfer, acoustics, electromagnetism, MEMS (Micro Electro Mechanical Systems), and etc. These programs can be classified as either "package" program or "single purpose" program. Single purpose programs usually have convenient and powerful functions, but these programs have limited expandability to different fields of analysis. Therefore, the method to converter the analysis results of single purpose program to other programs is needed. In the research, multi-body data conversion methods of 1) finite element model and 2) solid model were created to convert fluid analysis result of CFD-ACE+ to ANSYS data structure. Automatic boundary condition algorithms were developed for blade, and finite element model was compared with solid model. It is expected that, by sealess data transfer, the Multi-body Data Conversion Program could reduce the development period of torque converters.

• 한국산림과학회지
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• 제88권1호
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• pp.11-17
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• 1999

유묘상태에서 잡종을 판정하기 위해 수령에 따른 잎과 모용(毛茸)의 형태를 조사하였다. 졸참나무, 떡갈나무, 갈참나무에서 잎의 크기는 1년생묘에서 가장 작고, 수령의 증가에 따라서 커지는 경향을 보였다. 잎의 길이, 잎의 넓이, 잎자루 길이, 결각의 수, 결각의 깊이, 형상비, 잎자루 비율에 관하여서도 수령에 따른 차이가 관찰되었다. 이 때문에 1, 2년생의 유령기에 잎의 크기, 형태만으로 종을 판정하기는 어려웠다. 또한 잎 뒷면의 모용(毛茸)의 종류, 형상, 발생 밀도 등은 종에 따라서, 같은 종 중에서도 수령에 따라서 현저하게 차이를 보였다. 졸참나무의 성목은 소형성상모밀생(小型星狀毛密生) 장모소생형(長毛疎生型), 떡갈나무의 성목은 대형성상모밀생(大型星狀毛密生)~소생형(疎生型), 갈참나무의 성목은 소형성상모밀생형(小型星狀毛密生型), 일본 물참나무의 성목은 무모(無毛)~소형성상모산생형(小型星狀毛散生型)으로 성목에서는 모용(毛茸)으로 종의 판정이 가능하였다. 1, 2년생의 묘목에서는 모용(毛茸)의 발생이 좋지 않으며 졸참나무, 떡갈나무에서는 2년생 일부와 3년생에서 모용(毛茸)에 의해 종의 분류가 가능하였지만, 갈참나무 일본 물참나무에서는 유령기에 모용(毛茸)만으로서 종을 판정하기는 곤란하였다.

• 대한기계학회논문집B
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• 제20권10호
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• pp.3262-3271
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• 1996

Flow patterns were measured in a shrouded centrifugal impeller. The flow rate in measurements was fixed at the value corresponding to a nearly zero incidence at the blade inlet. By using a single slanted hot-wire probe and a Kiel probe mounted on the impeller hub disk, the 3-D relative velocities and the rotary stagnation pressures were measured in seven circumferential planes from the inlet to the outlet of impeller rotating at 700 rpm, and the static pressure distribution along flow passage and the slip factor at impeller outlet were calculated from the measured values. From these measured data, the primary and secondary flows, the wake production and the static pressure rise in the impeller passage were investigated. Furthermore, the secondary flow patterns and the wake's location in this impeller passage were compared with those of the unshrouded impeller.

• 한국추진공학회지
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• 제9권4호
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• pp.66-72
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• 2005

본 연구에서는 초음속 충동형 터빈의 유동특성을 알아보기 위해 소형 초음속 풍동을 설계하였으며 Single pass Schlieren system을 이용하여 유동을 가시화하였다. 실험은 2차원 초음속 노즐과 익렬을 조합하여 블레이드 앞전 형상과 노즐-익렬 간극에 따라 실시하였다. 실험을 통해 충격파를 포함한 복잡한 유동 형태와 노즐-익렬, 충격파-경계층 상호작용 등을 관찰할 수 있었다.

• 한국유체기계학회 논문집
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• 제15권6호
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• pp.77-84
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• 2012

The aerodynamic performance of a single-stage transonic axial compressor was experimentally evaluated by measuring pressure and temperature distribution at the inlet and outlet of the compressor. The compressor was developed by Korea Aerospace Research Institute through multidisciplinary design optimization (MDO) method, especially integrating aerodynamic performance and structural stability. The test results show that the pressure ratio is 1.65 and the efficiency is 85.8 % at design point, where the corrected speed is 22,000 rpm and the corrected mass flow rate is 15.4 kg/s, and it has a good agreement with the design target and computational results. The distribution of pressure ratio is very steep at design speed, compared with the trend of other subsonic compressors. Also the static pressure distribution on the stator casing shows that the blade loading is gradually increasing through the stage as designed.

• 대한기계학회논문집B
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• 제26권2호
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• pp.201-210
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• 2002

Experiments were done for performance and flow characteristics of a counter-rotating axial flow fan. Performance curves of a counter-rotating axial flow fan were obtained and compared by varying the blade pitch angles. The fan characteristic curves were obtained following the Korean Standard Testing Methods for Turbo Fans and Blowers (KS B 6311). The fan flow characteristics were measured using a five-hole probe and a slanted hot-wire. The velocity profiles between the hub and tip of the fans were measured and analyzed at the peak efficiency point. The peak efficiency of the counter-rotating axial flow fan was improved about 15% respectively, compared with the single rotating axial fan. The single rotating axial flow fan showed relatively law efficiency due to the swirl velocities behind rotor exit which produced pressure losses. The counter-rotating axial flow fan showed that the swirl velocity generated by the front rotor was eliminated by the rear rotor and the associated dynamic pressure is recovered in the from of the static pressure rise.

• 한국컴퓨터정보학회논문지
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• 제26권6호
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• pp.47-53
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• 2021

본 논문에서는 단일 팬 방식 홀로그램 디스플레이의 제한된 시야각 문제점을 개선하기 위한 멀티비전 기반 홀로그램 디스플레이를 제안한다. 기존 단일 팬 방식의 디스플레이는 시야각이 좁고 팬의 길이가 길어짐으로 인한 낮은 해상도의 문제점을 가진다. 또한, SD 카드 사용으로 인한 데이터 변경의 어려움을 Wi-Fi 방식으로 데이터를 송신하기 위한 전용 앱을 구현하고자 한다. 본 논문에서는 3개의 REG LED 팬으로 구성된 디스플레이를 설계하고 구현하였다. 앱을 이용한 영상송신 결과, 광고 및 시연 등의 상업적 용도로 사용할 수 있음을 확인하였다. 본 연구의 결과는 멀티비전 홀로그램의 대중화에 많은 도움이 될 것으로 사료된다.

• 한국산업융합학회 논문집
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• 제4권3호
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• pp.243-251
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• 2001

The effects of various operating parameters(agitation speed, impeller type, antiform agents, impeller spacing etc.) on air-liquid mass transfer was characterized by volumetric mass transfer coefficient($k_La$). Also, the dual-impeller agitated systems are compared with single-impeller agitated systems with a special focus on its applications for bioreactors, $k_La$ was take over a range of 200~450 rpm of agitation speed, and 0.5~2.5 vvm of air flow rates, for four single impeller and impeller combinations consisting of four impeller types, namely rushton, pitched blade, scaba, intermig were tested. The rushton impeller showed the best $k_La$ as compared with other single impellers. The dual impeller system are found to be superior as compared to single impeller in all aspects, The best combination of the dual impeller was a intermig of axial flow type as an upper impeller and a rushton of radial flow type as a lower part. Also, the control of the DO level with the variation of agitation speed was more efficient than that with an increase in air flow rate. The addition of antiform dropped the $k_La$ very large up to 1g/L regardless the type. PPG was less effect on $k_La$ than other antiforms. The impeller spacing and presence of solute are found very effective on $k_La$. When the $NaNO_3$is presented as solute, the $k_La$ increased approximately 50% then control.

• Nuclear Engineering and Technology
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• 제50권1호
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• pp.18-24
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• 2018

This study proposes a new method of analyzing the burnup credit in boiling water reactor spent fuel assemblies against various operating parameters. The operating parameters under investigation include fuel temperature, axial burnup profile, axial moderator density profile, and control blade usage. In particular, the effects of variations in one and two operating parameters on the curve of effective multiplication factor ($k_{eff}$) versus burnup (B) are, respectively, the so-called single and compound effects. All the calculations were performed using SCALE 6.1 together with the Evaluated Nuclear Data Files, part B (ENDF/B)-VII238-neutron energy group data library. Furthermore, two geometrical models were established based on the General Electric (GE)14 $10{\times}10$ boiling water reactor fuel assembly and the Generic Burnup-Credit (GBC)-68 storage cask. The results revealed that the curves of $k_{eff}$ versus B, due to single and compound effects, can be approximated using a first degree polynomial of B. However, the reactivity deviation (or changes of $k_{eff}$, ${\Delta}k$) in some compound effects was not a summation of the all ${\Delta}k$ resulting from the two associated single effects. This phenomenon is undesirable because it may to some extent affect the precise assessment of burnup credit. In this study, a general formula was thus proposed to express the curves of $k_{eff}$ versus B for both single and compound effects.