• 산업기술연구
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• 제30권A호
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• pp.17-23
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• 2010

Recently, a large number of open-pit mines are planning to change their mining method to underground types because the environmental concerns and legal regulations are increased with a rise in the standard of living. The K silica mine, which is one of them and located in Kyunggi province, is planning the establishment of a vertical shaft which will be used for ore-pass channel in their new glory hole mining method. This vertical shaft will be designed to join with a horizontal gangway excavated from the ground level. In this new mining system, the excavated ore particles will be stored inside a shaft and transported out with a help of a conveyor belt. Therefore the hang-up of ore particles in a shaft, the control of gate at the bottom of a shaft, the installation of dog-leg at the gate should be investigated identically. In this study, the PFC-2D code which is one of the discrete element numerical methods has been applied to simulate the particle flow mechanism in a shaft, and the optimum mine design has been proposed to maximize the productivity and to minimize the system damage.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.330-339
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• 2008

Ground-based interceptors(GBI) comprise a major element of the strategic defense against hostile targets like Intercontinental Ballistic Missiles(ICBM) and reentry vehicles(RV) dispersed from them. An optimum design of the subsystems is required to increase the performance and reliability of these GBI. Propulsion subsystem design and optimization is the motivation for this effort. This paper describes an effort in which an entire GBI missile system, including a multi-stage solid rocket booster, is considered simultaneously in a Genetic Algorithm(GA) performance optimization process. Single goal, constrained optimization is performed. For specified payload and miss distance, time of flight, the most important component in the optimization process is the booster, for its takeoff weight, time of flight, or a combination of the two. The GBI is assumed to be a multistage missile that uses target location data provided by two ground based RF radar sensors and two low earth orbit(LEO) IR sensors. 3Dimensional model is developed for a multistage target with a boost phase acceleration profile that depends on total mass, propellant mass and the specific impulse in the gravity field. The monostatic radar cross section (RCS) data of a three stage ICBM is used. For preliminary design, GBI is assumed to have a fixed initial position from the target launch point and zero launch delay. GBI carries the Kill Vehicle(KV) to an optimal position in space to allow it to complete the intercept. The objective is to design and optimize the propulsion system for the GBI that will fulfill mission requirements and objectives. The KV weight and volume requirements are specified in the problem definition before the optimization is computed. We have considered only continuous design variables, while considering discrete variables as input. Though the number of stages should also be one of the design variables, however, in this paper it is fixed as three. The elite solution from GA is passed on to(Sequential Quadratic Programming) SQP as near optimal guess. The SQP then performs local convergence to identify the minimum mass of the GBI. The performance of the three staged GBI is validated using a ballistic missile intercept scenario modeled in Matlab/SIMULINK.

• 공학논문집
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• 제2권1호
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• pp.113-123
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• 1997

이 논문은 위성 지구국용 수정곡면 카세그레인 안테나를 설계하는 것이다. 수정곡면 카세그레인 안테나 설계는 다음과 같은 절차로 수행된다. 1) 원하는 안테나 사양을 만족하도록 개구면 전계분포 설계, 2) 적절한 구조 퍼래미터 결정, 3) 반사판 곡면 좌표 추출 등이다. 이를 위해서 개구면 전계 분포는 Hansen 단일변수 분포를 선택하고, 개구면에 의한 원거리 복사패턴은 각스펙트럼법을 이용하여 예측한다. 설계 주파수에서 정해진 사양을 만족하도록 개구면을 설계한 후, 이 분포가 다른 주파수에서도 사양에 만족되는지 확인한다. 주어진 급전 패턴이 설계된 개구면 분포로 변환되도록 주 및 부반사판 곡면을 합성한다. 곡면추출에 필요한 급전 패턴으로 빔웨이브 가이드의 복사패턴을 이용한다. 설계된 시스팀은 원형 개구면을 갖고, 좌우 대칭이며, 축들이 기울어지지 않는 구조를 갖는다. 종합보간법을 이산적 반사판 설계 데이터들에 적용하여, 연속적인 반사판 곡면 함수를 얻는다. 기저 함수로 JPS함수를 사용한다. 설계는 주파수 17.7-20.2GHz의 수신밴드와 27.5-30GHz의 송신밴드를 갖는 Ka밴드에서 동작하는 카세그레인안테나를 설계한다.

• Structural Engineering and Mechanics
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• 제16권5호
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• pp.557-580
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• 2003

Laminated composite structures find wide range of applications in many branches of technology. They are much suited for weight sensitive structures (like aircraft) where thinner and lighter members made of advanced fiber reinforced composite materials are used. The orientations of fiber direction in layers and number of layers and the thickness of the layers as well as material of composites play a major role in determining the strength and stiffness. Thus the basic design problem is to determine the optimum stacking sequence in terms of laminate thickness, material and fiber orientation. In this paper, a new optimization technique called Cellular Automata (CA) has been combined with Genetic Algorithm (GA) to develop a different search and optimization algorithm, known as Cellular Genetic Algorithm (CGA), which considers the laminate thickness, angle of fiber orientation and the fiber material as discrete variables. This CGA has been successfully applied to obtain the optimal fiber orientation, thickness and material lay-up for multi-layered composite hybrid beams plates and shells subjected to static buckling and dynamic constraints.

• 한국해양공학회지
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• 제15권2호
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• pp.22-32
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• 2001

The numerical investigation of obliquely incident wave interactions with fully submerged dual buoy/porous-membrane floating breakwaters placed in parallel with spacing is studied based on linear potential theory and Darcy's law. The numerical solutions are obtained by using a discrete-membrane dynamic model and second-kind modified Bessel function distribution over the entire boundaries of fluid regions. First, numerical solutions for an idealized dual submerged system without buoys are obtained. Second, a more practical dual submerged system with membrane tension provided by buoys at its tops is investigated by the multi-domain boundary element method particularly devised for dual buoy/porous-membrane problems with gaps. The velocity potentials of wave motion are coupled with porous-membrane deformation, and solved simultaneously since the boundary condition on porous-membrane is not known in advance. The effects of varying permeability on membranes and wave characteristics are discussed for the optimum design parameters of systems previously studied. The inclusion of permeability on membrane eliminates the resonances that aggravate the breakwater performance. The system is highly efficient when waves generated by the buoys and membranes were mutually canceled and its energy at resonance frequency dissipates through fine pores on membranes.

• Structural Engineering and Mechanics
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• 제83권2호
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• pp.259-272
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• 2022

The branch of electronics that uses an organic solar cell or conductive organic polymers in order to yield electricity from sunlight is called photovoltaic. Regarding this crucial issue, an artificial intelligence-based predictor is presented to investigate the vibrational behavior of the organic solar cell. In addition, the generalized differential quadrature method (GDQM) is utilized to extract the results. The validation examination is done to confirm the credibility of the results. Then, the deep neural network with fully connected layers (DNN-FCL) is trained by means of Adam optimization on the dataset whose members are the vibration response of the design-points. By determining the optimum values for the biases along with weights of DNN-FCL, one can predict the vibrational characteristics of any organic solar cell by knowing the properties defined as the inputs of the mentioned DNN. To assess the ability of the proposed artificial intelligence-based model in prediction of the vibrational response of the organic solar cell, the authors monitored the mean squared error in different steps of the training the DNN-FCL and they observed that the convergency of the results is excellent.

• 한국건설관리학회논문집
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• 제10권3호
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• pp.102-110
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• 2009

동시공학 연구는 최근까지 국내에서 인식이 부족하여 잘 활용되지 못하였고 다만 패스트 트랙에 관한 연구가 활발히 진행되어 왔다. 그러나 본 연구는 기존의 패스트 트랙 방법에서 정량적인 분석과 논리적으로 증명 및 평가하는 연구가 미비하다고 판단하여, 상위 개념인 동시공학 방법을 분석하였다. 설계단계에서 정성적인 분석이 아닌 실제 예제를 통하여 정량적인 자료를 이용하여 각 공정별 중첩이 전체 프로젝트에 미치는 영향을 명확하게 보여주는 분석방법을 제시하였다. 시뮬레이션 기법을 이용한 정량적인 분석방법을 통하여 실제 분석 결과를 가지고 의사결정에 참고 자료로 활용이 가능하도록 하였다. 사례분석 결과 중첩 비율별 공기 비용 간의 관계를 알 수 있었고 중첩 비율별 값을 가지고 공기 비용간의 정량적인 분석을 통해 최적점을 제시함으로서 의사결정이 가능토록 하였다.

• 한국항공우주학회지
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• 제33권1호
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• pp.26-32
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• 2005

본 연구에서는 반응표면법에 다항함수, 지수함수, 로그함수등을 적용한 다양한 회귀함수를 이용하여 최적화를 수행하였다. 이를 검증하기 위해 트러스 구조와 하니콤 복합재 플랫폼에 대하여 응력 및 고유진동수를 고려하여 최적설계를 수행하였다. 근사함수를 효과적이고 용이하게 하는 방법을 실험계획법이라 하는데 중심합성법, 요인설계법, 회전계획법, 심플렉스법 등이 있으며, 본 연구에서는 중심합성법을 이용하여 반응표면을 생성하였다. 이를 위하여 구조해석 코드로 MSC/NASTRAN을 사용하였으며 최적설계 프로그램은 중심합성법을 기반으로 하여 다양한 회귀모델에 의한 반응표면을 적용하여 작성하였다. 또한 이 결과를 기존의 도함수를 이용한 최적화 기법이나 유전자알고리즘을 이용한 최적화 결과와 비교하여 반응표면법의 설계상의 장점 및 반응표면 생성 시 다양한 회귀모델에의 사용에 대한 신뢰성을 확인하였다.

• 한국터널지하공간학회 논문집
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• 제23권1호
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• pp.1-12
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• 2021

Tunnel boring machine (TBM)의 설계에 있어서 지반과 직접적으로 맞닿아 절삭을 담당하는 커터헤드의 설계에 따라서 장비의 굴진효율이 달라지게 된다. 디스크커터는 배치되는 위치에 따라 센터 커터 존, 이너 커터 존, 트렌지션 커터 존으로 구분된다. 기존에도 페이스커터의 최적 절삭조건을 규명하기 위한 연구는 많이 진행되어 왔으나, 트렌지션 커터의 최적 절삭조건을 규명하기 위한 연구는 상대적으로 미진하였다. 본 연구에서는 트렌지션 커터의 최적의 절삭조건을 규명하기 위해 개별요소법 수치해석을 수행하고 트렌지션 커터 사이의 각도에 따른 비에너지 곡선을 작도하여 최적 절삭조건을 알아보고자 하였다. 수치해석 결과 전이영역에서 최소 비에너지를 보이는 트렌지션 커터 사이의 각도 9°인 것으로 확인되었다. 이를 트렌지션 커터의 경사각에 따라 3가지 영역으로 구분하고 영역별 디스크커터 사이의 각도와 비에너지를 정리한 결과 트렌지션 커터의 경사각이 커질수록 최적 비에너지를 보이는 트렌지션 커터 사이의 각도는 10°에서 8°까지 점차 감소하는 경향을 보였다. 이러한 결과는 기존에 사용되고 있는 트렌지션 커터의 설계 결과와 유사한 경향으로써, 본 연구의 결과를 밑받침한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 춘계학술대회 논문집
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• pp.835-841
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• 2013

Modern solid-state gyroscopes (HRG) with hemispherical resonators from high-purity quartz glass and special surface superfinishing and ultrathin gold coating become the best instruments for precise-grade inertial reference units (IRU) targeting long-term space missions. Designing of these sensors could be a notable contribution into development of Korea as a space nation. In participial, 40mm diameter thin-shell resonator from high-purity fused quartz, fabricated as a single-piece with its supporting stem has been designed, machined, etched, tuned, tested, and delivered by STM Co. (ATS of Ukraine) several years ago; an extremely-high Q-factor (upto 10~20 millions) has been shown. Understanding of the best way how to match such a unique sensor with inner glass assembly of the gyro means how to use the high potential in a maximal extent; and this has become the urgent task. Inner quartz glass assembly has a very thin indium (In) layer soldered the resonator and its silica base (case), but effects of internal resonances between operational modal pair of the shell-cup and its side (parasitic) modes can notable degrade the potential of the sensor as a whole, instead of so low level of resonator's intrinsic losses. Unfortunately, there are special combinations of dimensions of the parts (so-called, "resonant sizes"), when intensive losses of energy occurs. The authors proposed to use the length of stem's fixture as an additional design parameter to avoid such cases. So-called, a cyclic scheme of finite element method (FEM) and ANSYS software were employed to estimate different combinations of gyro assembly parameters. This variant has no mismatches of numerical origin due to FEM's discrete mesh. The optimum length and dangerous "resonant lengths" have been found. The special attention has been paid to analyses of 3D effects in a cup-stem transient zone, including determination of a difference between the positions of geometrical Pole of the resonant hemisphere and of its "dynamical Pole", i.e., its real zone of oscillation node. Boundary effects between the shell (cup) and 3D short "beams" (inner and outer stems) have been ranged. The results of the numerical experiments have been compared with the classic model of a quasi-hemispherical shell band with inextensional midsurface, and the solution using Rayleigh's functions of the $1^{st}$ and $2^{nd}$ kinds. To guarantee the truth of the recommended sizes to a designer of the real device, the analytical and FEM results have been compared with experimental data for a party of real resonators. The consistency of the results obtained by different means has been shown with errors less than 5%. The results notably differ from the data published earlier by different researchers.