• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2018.11a
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• pp.216-217
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• 2018

소형 활주선의 경우, 대형 저속선 대비 항주자세의 변화가 크기 때문에 CFD 해석시 저항성능과 운동성능 결과에 오차가 발생할 수 있다. 본 연구에서는 Warped 2 선형을 대상으로 상용 CFD 코드인 STAR-CCM+ v9.04를 사용한 CFD해석을 수행하여, 이를 모형시험 결과와 비교하여 오차를 확인하였고, 또한 오차의 원인을 분석했을 때, 선체 하부의 Numerical ventilation 현상과 Spray 영역에 문제가 있다고 판단하였다. 추후 연구에서는 오차 해결 방법으로 VOF Phase replacement 기법과 Spray 영역에 대한 격자 최적화 방법을 연구하고자 한다.

• Journal of Ocean Engineering and Technology
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• v.15 no.3
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• pp.134-141
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• 2001

An experimental method to investigate the dynamic characteristics of buoys in extreme environmental condition is established. Because the buoy model requires a resonable size for accurate experiment, the test condition in model basin that satisfies the similarity law is hardly compatible with capability of test facilities. It is suggested that the linear wave component that is unable to satisfy similarity is separated with others. The model experiment is carried out with mitigated condition for the linear wave components while others including wave drift, current and wind are keeping the similarities. Then, the result can be extrapolated to give the dynamic behavior of buoys n extreme condition because linear wave component is solely responsibly to oscillatory buoy motion and other environmental components are applied as a initial tension. The similarity for current and wind conditions is viewed as equivalence of restoring forces. The validity of proposed method is examined with different types of standard ocean buoys and it indicates that the linearity of measured characteristics is assured with a limitation of resonable distance between test and estimated wave conditions.

• Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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• 2001.05a
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• pp.208-215
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• 2001

An experimental method to investigate the dynamic charasteristics of buoys in extreme environmental condition is established. Because the buoy model requires a resonable size for accurate experiment, the test condition in model basin that satisfies the similarity law is hardly met with capability of test facilities. It is suggested that the linear wave component that is unable to satisy similarity is separated with others. The model experiment can be carried out with mitigated condition for the linear wave components while others including wave drift, current and wind are keeping the similarities. Then the result is extrapolated to give the dynamic behavior of buoys in extreme condition because linear wave component is soley responsible to oscillatory buoy motion and other environmental components are applied as a initial tension. the similarity for current and wind conditions is viewed as equivalence of restoring forces. the validity of proposed method is examined with different types of standard ocean buoys and it indicates that the linearity of measured characteristics is assured with a limitation of resonable distance between test and estimated wave conditions.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.1
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• pp.66-72
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• 2007

an approach to air-vehicle design, an application of the radio-controlled model flight test techniques has been presented. The approach presented in this study is to validate the air-vehicle design configuration by analyzing the flight test results of scale model with dynamic similarities, and then to apply the analyzed results to the aerodynamic design process in early stage of the air-vehicle development. To develop practically applicable similarity laws for the subscale flying model design, the air-vehicle motions are decoupled into rotational motions for stability & control similarities and translational motions for flight performance similarities. Also, detail techniques for radio-controlled model flight test have been developed. Based on the results obtained from the radio-controlled flight test, the present approach for air-vehicle design has shown to be useful to validate the air-vehicle design configuration.

• Journal of Navigation and Port Research
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• v.32 no.10
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• pp.759-764
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• 2008

The planing craft is designed specifically to achieve comparatively high speed on the surface of the water. Most of planing crafts have installed the spray strip in decreasing of wave impaction and improving motion performance of rolling and pitching et al. It is known to reduce the spray and frictional resistance by the effect of lift and improvement of wave profile in high speed. In this paper, the high speed planing crafts with & without spray strip in bottom were performed to compare the resistance performance by model-test. In conclusion, the high speed planing crafts with spray strip in bottom was proved to effect of the resistance decrement of $3.0{\sim}5.0%$.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.04a
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• pp.16-19
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• 2011

An experimental study on the spray characteristics of Gas-centered swirl coaxial injectors(GCSCI) for high-performance staged combustion rocket engines has been carried out using cold flow tests. In this study, water and gaseous nitrogen are used as working fluids and a back-lit photography technique with image processing for the measurements of spray characteristics. Our study is focused on the effect of injector geometries like as gap thickness of liquid nozzle and gas nozzle and momentum flux ratio for fundamental understanding of the injectors.

• Rubber Technology
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• v.11 no.1
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• pp.12-26
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• 2010

각종 산업제품의 주요 부품으로 사용되고 있는 고무재료는 사용 중 온도변화에 의해 체적 또는 길이 변화를 수반할 수 있어 결과적으로 고무제품의 성능이나 효율이 영향을 받게 된다. 특히 고온에서 고무제품의 치수변화를 제한하거나 일정치수를 강제할 경우 열수축이나 열팽창에 의해 응력이 발생하게 된다. 따라서 온도 변화에 따른 열응력의 측정은 고무제품의 정밀성과 성능을 평가하는 중요한 수단을 제공한다. 본 연구에서는 고무소재의 열응력 측정을 위한 새로운 측정방법을 개발하였고 이와 관련 새로운 시험장치를 설계, 제작하였다. 고무시편에 일정 변형의 인장을 준 상태에서 가열하면 열응력이 발생한다. 이 때의 열응력은 고무분자 사슬들의 운동성에 기인하며 배향된 고무분자 사슬들이 열역학적으로 랜덤 사슬형태로 돌아가려는 엔트로피적 힘이다. 따라서 온도가 높을수록 그 수축력은 증가하게 된다. 또한 고무분자 사슬의 사전 변형이 증가하면 그 열응력은 증가한다. 이때 열응력은 측정시간이 지남에 따라 최대치에 도달한 후 완화되며 그 완화속도는 설정온도에 의해 영향을 받는다. 여기서는 온도변화에 따른 고무시편의 열응력 측정결과를 소개하고, 고무분자 사슬의 엔트로피 변화와 점탄성적 흐름, 그리고 가열에 따른 고무 시편의 팽창 또는 수축이 열응력에 미치는 영향 등을 논의하였다. 특히 천연고무와 SBR 고무시편의 열응력 차이를 분자사슬의 운동과 연관하여 검토하였고, 가교밀도와 가교시스템이 각각 다른 고무시편에 대해 열응력 발생과에 따른 상관관계를 고찰하였다. 또한 시편의 형태와 두께가 열응력 발생에 미치는 영향도 검토하였다. 충전 배합고무의 경우 열응력에 영향을 미치는 인자로 고무분자 사슬의 운동성과 가교밀도 외에 고무재료와 충전제 사이의 물리 화학적 상호작용도 매우 중요한 요소가 된다. 배합고무에서 충전제의 영향을 검토하기 위해 실리카와 카본블랙을 선택하였고 배합고무의 열응력을 각각 측정하여 이들의 보강효과가 열응력에 미치는 영향에 대해 논하였다.

• Journal of rehabilitation welfare engineering & assistive technology
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• v.3 no.1
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• pp.41-47
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• 2009

This paper describes requirements and test methods for the safety of electromyographs and evoked response equipments to be used for medical examination of the central nerve system and motor-sensory functions in cortex. We first establish internationally harmonized requirements for the safety, and then propose a test procedure and test methods corresponding to the requirements based on the international standards. However requirements for the performance of each equipments are not specified in order to admit maker's specifications. Using a electromyography equipment we verified validity of the test methods proposed. Results of this study can be used as a standard for approval of Korea Food and Drug Administration (KFDA).

• Journal of the Korean Society for Marine Environment & Energy
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• v.4 no.1
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• pp.70-74
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• 2001

In this paper, we studied the maneuvering performances of a ship with flapped rudder. PMM tests were carried out for a ship model with horn type rudder or flapped rudder. The Abkowitz's model was used as a basic mathematical model to simulate the maneuvering motions. The maneuvering motions of a ship with flapped rudder were compared with those of a ship with horn-type rudder. As a result, it was found that the turning ability of a ship with flapped rudder was remarkably improved.

• Journal of the Korean Society of Propulsion Engineers
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• v.3 no.4
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• pp.38-43
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• 1999

An experimental study was carried out, in order to set up the procedure for evaluation of hot fire test, to investigate the effect of mixture on combustion performance and combustion stability , and to determine the optimum design condition for designing the liquid rocket engine. $HNO_3$/Kerosene uni-element liquid rocket engine(thrust 24 $\iota{b}_f$, chamber pressure 200 psia) using impinging streams doublet injector was designed, and ground hot-fire test was carried out. To prevent or reduce the hard start during ignition period, two step ignition method was used. This was accomplished by maintaining about 25% of the designed operating pressure doting transient period, then chamber pressure was built up to the designed operating pressure. Maximum combustion efficiency was at O/F ratio 3.6, and combustion efficiency is decreased with increasing momentum ratio.