• Proceedings of the Computational Structural Engineering Institute Conference
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• 2010.04a
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• pp.746-749
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• 2010

본 연구에서는 비보강 조적조에 대한 부재 비선형거동 및 비탄성힌지 속성을 고려할 수 있는 midas GEN Ver.741(해외판) 프로그램에 의한 비보강 조적벽체의 푸쉬오버 해석결과와 실험결과와의 비교를 통하여 비보강 조적조 건축물의 전단강도평가를 비롯하여 내진성능평가를 위한 역량스펙트럼 해석 프로그램을 검증하고자 한다. midas GEN Ver.741(해외판) 프로그램의 사용성 검증을 위하여 조적벽체의 축하중, 형상비, 쌓기방법(두께) 그리고 개구부 유무를 변수로 한 10개의 비보강 조적벽체의 전단강도를 비교 평가한다. 비보강 조적벽체에 대한 실험결과와 해석결과를 비교한 결과 각 시험체별 전단강도 값이 비교적 유사한 것으로 나타나며 국내 기존 비보강 조적조 건축물에 대한 해석방법으로 본 프로그램의 사용이 가능한 것으로 평가되었다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2007.11a
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• pp.159-162
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• 2007

뉴테이션(Nutation, 장동)은 자이로스코프와 같은 큰 축 대칭 물체의 회전축에 대해 작은 불규칙적인(어원적으로 "nodding") 운동이다. 위성체가 회전상태에 돌입하게 될 때 위성체가 순수한 회전 운동이 아닌 뉴테이션 운동을 일으킬 경우, 이를 제거하기 위하여 뉴테이션댐퍼(NutationDamper)를 사용한다. 유도탄에 들어가는 부품 중에서 자이로조립체 내에 들어 있는 뉴테이션댐퍼의 개발을 하고자 본 연구를 수행 하게 되었으며, 자이로조립체 내에서 뉴테이션댐퍼의 역할은 자이로조립체의 원주상에 환형 튜브 형상으로 장착되어 자이로조립체가 세차운동(Precession)을 할 때 부가적으로 수반되는 바람직하지 못한 떨림(Wobble motion)인 뉴테이션을 감쇠시키는 기능을 수행한다.

• Aerospace Engineering and Technology
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• v.6 no.1
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• pp.114-119
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• 2007

This paper introduces modal test of the 2nd stage structure of KSLV-I which is composed to satellite, PLA(Payload Adapter), EB(Equipment Bay), KMS(Kick Motor Support) and KM(Kick Motor) without PLF(Payload Fairing). In this test, to simulate free-free boundary condition, test object was hung by 4 bungee cords and excited by using impact hammer. From this test, dynamic properties of the 2nd stage structure of KSLV-I can be obtained. Modal test data are analyzed by using TDAS(Test Data Analysis Software). As the result, modal parameters and mode shapes below 100Hz of the 2nd stage of KSLV-I were identified.

• Journal of the Korean Geotechnical Society
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• v.27 no.6
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• pp.27-37
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• 2011

Recently, pressure grouting is widely being used in construction site for strength improvement of ground and water proof, reinforcement and so on. It is necessarily required to estimate an appropriate injection pressure and injection time for economical and reasonable construction in the site through the size and shape of the hardened grout measured according to ground condition. However, sampling for the hardened grout is time-consuming and needs high cost on preliminary test in the site. The system which could predict the size and shape of the hardened grout does not exist until now. Thus, numerical method based on VOF method and porous model was used for the calibration chamber injection test with injection pressure (50 kPa, 100 kPa, 150 kPa) in this study. The results indicate that the numerical technique based on VOF method and porous model among CFD analysis is expected to be a basic study for the prediction of the behavior and solidification of pressure grouting.

• Tunnel and Underground Space
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• v.17 no.5
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• pp.389-410
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• 2007

For moderately jointed to massive rock masses, the failure and deformation behaviors around an excavated opening are absolutely influenced by the initial rock stress and strength of in-situ rock mass. The localized and progressive brittle failure around an opening does not mean whole collapse of an excavated opening. But, for many cases, it may induce temporary stopping of excavation works and reexamination of the current supporting system, which can result in delay of the entire construction works and additional construction cost. In this paper, the characteristics of the brittle failure around an opening with stress level and tunnel shape was studied by the biaxial compressive test using scaled specimen and by the numerical simulation with $PFC^{2D}$. The biaxial test results were well coincided with the stress induced failure patterns around the excavated openings observed and monitored in the in-situ condition. For the circular part of the opening wall, the stress induced cracks initially occurred at the wall surface in the direction of the minimum principal stress and contributed to the localized notch shaped failure region having a certain range of angle. But for the corner and straight part of the opening wall, the cracks initiated at sharp corners were connected and coalesced each other and with existing micro cracks. Further they resulted in a big notch shaped failure region connecting two sharp corners.

• Magazine of the Korea Concrete Institute
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• v.4 no.1
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• pp.81-87
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• 1992

In this thesis, the fatigue tests were performed on a series of SFRC(steel fiber reinforced concrete) to investigate the fatigue behavior of SFRC varying with the steel fiber contents and the steel fiber aspect ratios. The three point loading system is used in the fatigue tests. In tl1ese tests, relations between the repeated loading cycles and the mid-span deflections, number of repeated loadmg cycles when specimen was fractured were observed. On this basis, the mid-span deflections, the elastic strain energy and inelastic strain energy of SFRC were studied. A S - N curve \vas drawn to present the fatigue strength of SFRC beam. From che test results, by increasing the steel fiber content the energy lost on the permanent deformation decreases and the energy spent on crack growth increases. But in case of SFRC with the same steel fiber content the higher the steel fiber aspect ratio is, the less the elastic strain energy is. According to S - N curve drawn by the regression analysis on the fatugue test results, the fatigue strength with 2,000,000 repeated loading cycles in SFRC with the steel fiber content is 1.0% shows about 70% on the first crack static flexural strength.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2012.05a
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• pp.293-294
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• 2012

탄소섬유 복합재의 기계적 강도를 높이기 위하여 탄소섬유상에 ZnO 나노구조체를 도금하는 연구를 수행하였다. 전기도금을 이용하여 정전위법으로 탄소섬유상에 ZnO 나노구조체를 도금시킨 후 에폭시 YD-128과 경화제 KBH1089를 이용하여 탄소섬유 복합재를 제작하였다. 제작된 탄소섬유 복합재는 실험규격 ASTM D2344를 준수하였으며 ILSS(Interaminar Shear Strength)시험으로 강도를 측정하였다. 본 연구결과 탄소섬유에 인가되는 coulomb양을 조절함으로서 ZnO 나노구조체 형상을 제어할 수 있었으며, 일반탄소섬유 복합재와 ZnO 나노구조체가 도금된 탄소섬유 복합재의 강도를 비교하였을 때 ZnO 나노구조체가 도금 된 탄소섬유 복합재에서 더 높은 강도 값을 얻을 수 있었다.

• Journal of the Korean GEO-environmental Society
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• v.24 no.9
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• pp.15-24
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• 2023

The behavior of buried pipes is directly influenced by the nonlinearity and complex characteristics of the surrounding soil. However, the simplified beam-spring model, which ignores the nonlinearity and complex behavior of soil, is commonly used in practice. In response, several studies have employed continuum analysis methods to account for the nonlinear and complex behavior of the soil. This paper presents various numerical continuum analysis techniques and verifies their comparison with full-scale tests. The study found that reaction force results close to the full-scale test could be obtained by applying contact surface characteristics that take into account the interaction between the ground and the buried pipe. In the case of sharing pipe and soil node method and ignoring the interaction between pipe and soil, excessive reaction force was derived, and the failure shapes were different. In addition, this study applied the dynamic explicit analysis method, ALE method, and CEL method. It was confirmed that the displacement-reaction relationship and failure shape are similar to those of the static analysis.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.9
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• pp.607-616
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• 2019

Free body diagram analysis is done for key parts of pilot stage of LLV (Load Limit Valve) which is used to protect overload for static structural test of aerospace flight vehicle. It is shown through the analysis that diameter ratio($D_2)^{ten}/D_2)^{comp}$) of two poppets in a pilot stage must be equal to piston area ratio($A_{comp}/A_{ten}$) of a hydraulic actuator for making a poppet open consistently at constant force applied by an actuator. The result of the analysis is verified by measuring geometries of the poppets in the four different LLVs which are corresponding to four actuators with different capacity and have been used after being imported in this laboratory. Results of "Adjuster resolution tests" with two different pilot stages show the max. deviation of Fi(actuator force in instant of opening poppet) from average Fi obtained for each turn of adjuster is 0.3KN and max. deviation of the Fi normalized by average Fi of each turn of adjuster is 3.7%. From the results, it is verified that the two pilot stages with same poppet diameter ratio make a poppet consistently open at Fis within ${\pm}3.7%$ deviation from the average Fi. The deviation is shown to be caused from frictional force of O-ring in the poppet. Additionally, design factors for poppet spring and adjuster, which are also key parts of the pilot stage, are distinguished and procedure for deciding the factors are also shown in this study.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.164-167
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• 2003

In generally, Gas fill & drain valve is used in filling Gases to tank on high pressure in launcher The valve is quick coupling type and is separated by manual or remote control. In KSR-III, He gas fill & drain valve separated by remote control is used. In this paper, that are explained about the design specification, the test procedure, the autonomous test result and the flight test result.