• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2000년도 가을 학술발표회 논문집
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• pp.201-208
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• 2000

In this study, the behavior of saturated sandy soils under dynamic loads - pore water pressure and effective stress - was investigated using Disturbed State Concept(DSC) model. The model parameters are evaluated from laboratory test data. During the process of loading and reverse loading, DSC model is utilized to trace strain-hardening and cyclic softening behavior. The procedure of back prediction proposed in this study are verified by comparing with laboratory test results. From the back prediction of pore water pressure and effective mean pressure under cyclic loading, excess pore water pressure increases up to initial effective confining pressure and effective mean pressure decrease close to zero in good greement with laboratory test results. Those results represent the liquefaction of saturated sandy soils under dynamic loads. The number of cycles at initial liquefaction using the model prediction is in good agreement with laboratory test results. Therefore, the results of this study state that the liquefaction of saturated sandy soils can be explained by the effective tress analysis.

• Communications for Statistical Applications and Methods
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• 제9권1호
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• pp.229-240
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• 2002

Whether to use linear or quadratic model in the analysis of regression data is one of the important problems in classical regression model and measurement error model (MEM). In MEM, four goodness of fit test statistics are available In solving that problem. Two are from the derivation of estimators of quadratic MEM, and one is from that of the general $k^{th}$-order polynomial MEM. The fourth one is derived as a variation of goodness of fit test statistic used in linear MEM. The purpose of this paper is to find the most powerful test statistic among them through the small-scale simulation.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2009년도 세계 도시지반공학 심포지엄
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• pp.1011-1016
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• 2009

In this study, to performed laboratory model tests in order to verify on load transfer condition of drilled shaft under lateral loading. To conducted model test on polystyle drilled shaft under multi layer ground conditions. In model test, to measured the strain of drilled shaft and displacement under later loading. In order to verify on model test results, to conduct the numerical analysis.

• 한국항해항만학회지
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• 제33권9호
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• pp.603-608
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• 2009

In this paper, a 3m-class free running model ship will be introduced with its manoeuvring performance experiments. The results of turning circle test and zig-zag test will be explained. The developed system are equipped with GPS, main control computer, wireless LAN, IMU (Inertial Measurement Unit), self-propulsion propeller and driving rudder. Its motion can be controlled by RC (Radio Control) and wireless LAN from land based center. Automatic navigation is also available by pre-programmed algorithm. The trajectory of navigation can be acquired by GPS and it provides us with important data for ship's motion control experiments. The results of manoeuvring performance experiment have shown that the developed free running model ship can be used to verify the test of turning circle and zig-zag. For next step, other experimental researches such as ship collision avoidance system and automatic berthing can be considered in the future.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2006년도 추계 학술발표회 논문집
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• pp.125-128
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• 2006

Many research have been carried out concerned with the flexural performance of FRP composite in a various ways. Most of them, however, have used a small-scale specimen, so haven't been fully verified by full-scale model test. In this study, a full-scale RC beam model test for flexural strengthening with CFRP composites has been performed in order to verify test results obtained through a series of small-scale model test with respect to FRP stiffness affecting strengthening performance in the previous studies. A total of 4 specimens have been manufactured including control beam. The specimens strengthened with CFRP composites consist of 3 different CFRP stiffness with 2 types of CFRP composite. Consequently, the purpose of this study is to estimate influence of the size effect of specimens and FRP stiffness on the flexural performance. As a result, the effective strain of FRP composite is inversely proportional to FRP stiffness and ensures the same performance with small-scale model test.

• 한국군사과학기술학회지
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• 제25권4호
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• pp.355-363
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• 2022

Development of supersonic flying vehicle is one of the most latest issue in modern military technology. Specifically, structural integrity of supersonic flying vehicle can be verified by high temperature structural test. High temperature structural test is required to consider thermal load caused by aerodynamic heating while applying structural load simultaneously. Tubular quartz lamps are generally used to generate thermal load by emitting infrared radiation. In this study, modified heat flux model of tubular quartz lamp is proposed based on existing model. Parameters of the proposed model are optimized upon measured heat flux in three dimensions. Finally, thermal load of plate specimen is designed by the heat flux model. In conclusion, it is possible to predict heat flux applied on plate specimen and desired thermal load of high temperature structural test can be obtained.

• Structural Engineering and Mechanics
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• 제67권5호
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• pp.505-516
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• 2018

In this paper, the effects of particle size and model scale of concrete has been investigated on the failure mechanism of PFC2D numerical models under uniaxial compressive test. For this purpose, rectangular models with same particle sizes and different model dimensions, i.e., $3mm{\times}6mm$, $6mm{\times}12mm$, $12mm{\times}24mm$, $25mm{\times}50mm$ and $54mm{\times}108mm$, were prepared. Also rectangular models with dimension of $54mm{\times}108mm$ and different particle sizes, i.e., 0.27 mm, 0.47 mm, 0.67 mm, 0.87 mm, 1.07 mm, 1.87 mm and 2.27 mm were simulated using PFC2D and tested under uniaxial compressive test. Concurrent with uniaxial test, direct shear test was performed on the numerical models. Dimension of the models were $75{\times}100mm$. Two narrow bands of particles with dimension of $37.5mm{\times}20mm$ were removed from upper and lower of the model to supply the shear test condition. The particle sizes in the models were 0.47 mm, 0.57 mm, 0.67 mm and 0.77 mm. The result shows that failure pattern was affected by model scale and particle size. The uniaxial compressive strength and shear strength were increased by increasing the model scale and particle size.

• 정보처리학회논문지D
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• 제17D권4호
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• pp.283-296
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• 2010

Timing diagram은 시스템의 사양을 작성하는 도구로 많이 사용되고 있으나, Timing diagram을 이용하여 테스트 케이스를 생성하는 연구는 존재하지 않는다. 이와 같은 문제를 해결하기 위해 본 연구에서는 Timing diagram 으로부터 테스트 케이스를 생성하기 위해 다음과 같은 과정을 거쳤다. 1) Timing diagram을 형식적으로 기술하였다. 2) 정의된 Timing diagram의 의미로부터 이와 동치 관계에 있는 Stateflow 모델로 변환하는 방법을 기술하였다. 3) 변환된 Stateflow 모델에 대해 Simulink의 플러그 인 되어 있는 도구인 SDV를 사용하여 테스트 케이스를 생성했다. 이 접근 방법이 유용함을 보이기 위해서 도난 경보 모델과 임의의 Timing diagram모델들을 대상으로 실험을 수행하였다. 실험에서 Timing diagram 모델들로부터 Stateflow모델들로 변환하고 이를 SDV를 사용하여 테스트 케이스를 생성하였으며 그 결과에 대해 분석하였다. 이 연구를 통해 얻을 수 있는 결론은 Timing diagram이 더 이상 사양서를 작성하는 도구로만 사용되는 것이 아니라 모델 기반의 테스트 케이스를 생성하고자 하는 경우에도 유용한 도구가 된다는 점이다.

• 대한조선학회논문집
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• 제55권1호
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• pp.28-36
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• 2018

The experimental results of the model tests for the twin propeller cavitation noise are presented. The model test was carried out by means of procedure of noise measurement followed by the signal processing and full-scale extrapolation. In order to convert the measured sound pressure level into the sound source level, transfer function measurements for three conditions were performed according to the combination of locations and number of virtual sources. White noise and LFM signal were used as a source signals to examine the influence of the input signal. For the twin propellers, 5 transfer functions were defined and the results were discussed. Cavitation noise measurement tests were performed similarly to the transfer function measurement test. Noise source localization analysis was performed to confirm the test effectiveness. It was confirmed that the source level of the twin propeller can be estimated reliably by using transfer function corrections. Finally, the model test results were converted into full-scale by applying the ITTC '87 model-ship scaling raw, and the validity of the model test was confirmed by comparison with the full-scale measurement result.

• 터널과지하공간
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• 제29권6호
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• pp.425-438
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• 2019

본 연구에서는 일정한 방향의 층리가 발달한 퇴적암에 굴착된 지하철 병설터널을 모델링하여 축소모형 실험을 실시하였다. 연구대상 터널의 규격은 6.2 m×6.8 m이고 필러 폭은 4 m이다. 차원해석을 통해 현장암석에 적합한 모형재료를 선정하였고, 이를 사용하여 이방성 모형시험체를 제작하였으며 이축압축시험을 통해 터널의 파괴 및 변형거동을 알아보았다. 모형시험체에 하중을 증가시킴에 따라 필러의 중앙부에서 병설터널 사이를 가로지르는 최초의 균열이 발생하였고, 터널 천정부와 바닥부에서도 점차 파괴가 진행되었다. 필러부의 모든 균열은 기존의 층리면을 따라 발생하여 암반의 층리면이 필러 파괴의 주요 원인으로 나타났다. 또한, FLAC의 유비쿼터스 절리모델을 사용하여 실험 조건에 대한 수치해석을 실시함으로써 실험의 결과를 검증해 보았다. 여기서 얻어진 소성영역의 분포경향은 모형실험의 결과와 대체로 부합하여 실험의 신뢰성을 확인하였다.