• Proceedings of the Korea Concrete Institute Conference
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• 2009.05a
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• pp.439-440
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• 2009

Super high strength concrete tends to have compact tissue structure, and to have large reduction of volume by hydration reaction or large shrinkage by autogenous shrinkage. Thus, this study conducted basic research on the control of autogenous shrinkage of super high strength concrete using gypseous expansive additive.

• Proceedings of the Korean Society of Machine Tool Engineers Conference
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• 2003.10a
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• pp.277-282
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• 2003

The growth-strain method was applied to cutout optimization in laminated composite plates. Since the growth-strain method optimizes a shape by generating the bulk strain to make the distributed parameter uniform, the distributed parameter was chosen as Tsai-Hill value. In this study, of particular interest is to see whether the growth-strain method developed for shape optimization in isotropic media would work for laminated composite Plates. In volume control of the growth-strain method, it makes Tsai-Hill value at each element uniform in laminated composite plates under the predetermined volume. The shapes optimized by Tsai-Hill fracture index were compared with those of the initial shapes for the various load conditions and predetermined volumes of laminated composite plates. As a result, it was verified that volume control of the growth-strain method worked very well for cutout optimization in laminated composite plates.

• Journal of the Korea Institute of Military Science and Technology
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• v.19 no.2
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• pp.145-154
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• 2016

In this paper, a pneumatic device for the deployment performance verification of canards deployed by inertia has been designed and the performance of the pneumatic device has been proven through analysis and tests. The pneumatic conveying process, orifice opening process and piston movement process of the pneumatic device were investigated by using numerical methods. The orifice diameter, pressure in a pressure tank and type of gas were regarded as the main design parameters of the pneumatic device. The error rate between analysis and test results under the same conditions was within 4 %. The accuracy of numerical methods used in this study were validated.

• Journal of the Korea Institute of Military Science and Technology
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• v.13 no.3
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• pp.365-371
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• 2010

The fins of a missile which is folded within a canister are deployed according to a command during the missile flight. The aerodynamic load generated by operating environments such as missile flight speed, platform movement speed and wind acts as an anti-deploying force and prevents the fins from deploying. As the diversification of platforms and the higher speed of missiles need a larger deploying force but the space for operating the fin deploying device is getting narrower, the new design concepts are required for developing such a device. In this study, a pneumatic device for deploying missile fins is designed and its characteristics are verified through experiments and analyses.

• Proceedings of the KAIS Fall Conference
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• 2001.05a
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• pp.129-134
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• 2001

본 논문에서는 자동차 계기판 지시계 구동용 액츄에이터 연구의 일환으로써 소형 2상 스텝모터에 대하여 유한요소 수치해석을 이용한 설계, 해석 및 One Chip을 이용한 유량, 온도, RPM 및 속도 지시계 동시제어용 전용 구동 IC를 설계하였다. 일반적으로 자동차 계기판에 사용되어지고 있는 지시계의 구동원으로 코일형의 액츄에이터를 사용하고 있으나, 동작구간내의 선형성 및 속응성 저하와 구조상 큰 체적으로 인한 공간확대의 문제가 야기되어지고 있다. 따라서, 본 연구에서는 고 에너지 밀도를 갖는 소형의 영구자석과 저 손실 특성을 갖는 정밀 기어부 설계를 통하여 경량. 박형의 PM형 스텝모터를 설계하였으며. 또한 다수 모델 제어용 전용 드라이버 IC 설계 및 제작을 하였다. 실제로 제작한 모델을 대상으로 특성평가를 행하였으며, 이로부터 높은 선형성 및 고정밀도와 저소음 특성을 갖는 자동차 계기판 지시계용 구동원 및 드라이버의 활용 가능성을 확인 할 수 있었다.

• Proceedings of the Korean Powder Metallurgy Institute Conference
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• 2003.04a
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• pp.34-34
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• 2003

전기설()폭발(Electric Wire Explosion)법은 고밀도 전류를 금속와이어에 인가시키면 저항 발열에 의해서 금속와이어가 빠르게 가열되고, 수$\mu$sec 이내에 초기체적에 비해 2~3배나 팽창한 후 폭발하는 현상을 이용하여 나노분말을 제조하는 방법으로써, 다른 제조방법에 비해 값싼 비용으로 1~50$\mu$sec의 짧은 시간동안 극히 높은 온도($10^4~10^6K$)에 도달하기 때문에, 와이어 전체가 동시에 기화하여 원재료의 조성을 갖는 분말의 합성이 가능하며, 공급되는 에너지와 시간, 챔버의 용적과 압력을 제어함으로써 평균 분말 크기를 조절할 수 있다는 잇점이 있다. 또한, 금속 와이어 주위의 분위기를 조절함으로써 금속나노분말뿐만 아리나 산화물$\cdot$질화물$\cdot$탄화물 분말, 합금 분말, 화학적 화합물이나 복합재료 나노분말들을 만들 수 있어서 여러 산업분야에 대한 응용이 크게 기대되고 있다. 본 연구에서는 전기선()폭발 챔버(Fig. 1) 와 최대 20kV까지 제어 가능한 고출력 펄스 전원장치를 자체 제작하고, 이를 이용하여 은(Ag)나노분말 합성에 대한 실험을 행하였다. 이렇게 제조된 분말은 SEM, XRD, PSA, BET 등을 이용하여 비교분석 하였다.

• Transactions of the Korean Society of Automotive Engineers
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• v.8 no.2
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• pp.151-158
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• 2000

The growth-strain method was used for shape optimization of multi-connected structures. It was verified that the growth-strain method is very effective for shape optimization of structures with only one free surface to be deformed. But it could not provide reasonable optimized shape for multi-connected structures, when the growth-strain method is applied as it is. The purpose of this study is to improve the growth-strain method for shape optimization of multi-connected two- and three- dimensional structures. In order to improve, the problems that occurred as the growth-strain method was applied to multi-connected structures were examined, and then the improved method was suggested. The effectiveness and practicality of the developed shape optimization system was verified by numerical examples.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.310-313
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• 2006

The present study aims at investigating the effectiveness of a new passive cavity flow control technique, sub-cavity. The characteristics of cavity flow oscillation with the device are compared with those with other control techniques tested previously, including a triangular bump and blowing jet. In the computation, the three-dimensional, unsteady Navier-Stokes equations governing the supersonic cavity flow are solved based on an implicit finite volume scheme spatially and multi-stage Runge-Kutta scheme temporally. Large eddy simulation (LES) is carried out to properly predict the turbulent features of cavity flow. The present results show that the pressure oscillation near the downstream edge dominates overall time-dependent cavity pressure variations, and the amplitude of the pressure oscillation can be reduced in the presence of a sub-cavity.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.25 no.5
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• pp.850-856
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• 2001

Even though the hydraulic servo system has been widely used in industrial and military equipments since it has a lot of advantages, it is not easy to design controller due to the high nonlinearities and the parametric uncertainties. The dynamic behavior of the real process in the hydraulic servo system differs from that described by its model because the model is linearized. Another reason of the difference is caused by the variety of parameters, since the system parameters of the dynamic equation are affected by the operating conditions such as temperature and pressure. In this study, the designing process of the MRNC with a PID compensator is introduced and applied to the load sensing hydraulic servo system. The results show that the designed controller guarantees the robust control performance despite of both the nonlinearities and the parametric uncertainties.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.5
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• pp.101-108
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• 2002

A numerical simulation of an incompressible cavity flow is conducted. Two dimensional Navier-Stokes equations are integrated using staggered grid and a finite volume method with C-QUICK scheme for spatial derivatives and fully implicit scheme for the time derivatives. SIMPLE-C algorithm is employed to solve the pressure field. Computational results show that the third eddy is generated in the shear layer mode but not in the steady mode. This signifies that the third eddy plays an important role in cavity flow stability. As a means to control the flow, jet blowing is applied to a position below the cavity upstream edge. Effects of flow control parameters on the stability such as the frequency, the phase, and the velocity magnitude are reported.