• Journal of the Korea Concrete Institute
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• v.27 no.4
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• pp.419-426
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• 2015

The purpose of this study is to investigate experimentally the optimum mix design and site application case of soil mixing wall (SMW) method which is cost-effective technique for construction of walls for cutoff wall and excavation support as well as for ground improvement before constructing LNG storage tank typed under-ground. Considering native soil condition in site, main materials are selected ordinary portland cement, bentonite as a binder slurry and also it is applied $1,833kg/m^3$ as an unit volume weight of native soil, Variations for soil mixing wall are as followings ; (1) water-cement ratio 4cases (2) mixing velocity (rpm) 3levels (3) bleeding capacity and ratio, compressive strength in laboratory and site application test. As test results, bleeding capacity and ratio are decreased in case of decreasing water-cement ratio and increasing mixing velocity. Required compressive strength (1.5 MPa) considering safety factors in site is satisfied with the range of water-cement ratio 150% below, and test results of core strength are higher than those of specimen strength in the range of 8~23% by actual application of element members including outside and inside in site construction work. Therefore, optimum mix design of soil mixing wall is proposed in the range of unit cement $280kg/m^3$, unit bentonite $10kg/m^3$, water-cement ratio 150% and mixing velocity 90rpm and test results of site application case are satisfied with the required properties.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.8
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• pp.555-563
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• 2020

Foward-swept wings are known to possess superior aerodynamic performance compared to the conventional straight wings. However major concerns regarding forward-swept wings include divergence at lower airspeeds which require careful consideration at the design stage. As an endeavor to overcome such drawbacks, aeroelastic tailoring is attempted. In order to find an optimal ply sequence, recursive aeroelastic analyses is conducted and one-dimensional beam analysis coupled with simple aerodynamics is used for the improved computational efficiency and modelling convenience. The analysis used in this paper, DYMORE and analytic formula, both use one-dimensional beam model for the structure. Cross-sectional analysis for multi-cell NACA0015 airfoil section is conducted using VABS and oblique function is used for the sweep angle. Throughout the present aeroelastic tailoring, the maximum divergence speed of 290.2m/s is achieved which is increased by approximately 43% than that for the conventional ply configuration.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.10 no.2
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• pp.23-38
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• 1990

In this study, decompositive optimization method of two levels was selected to optimize effectively the geometry of the truss which takes the multi-loading condition, and the allowable stress, bucking stress, displacement and natural frequency constraints into consideration. The algorithm of this study is made up of sectional optimization using the feasible direction method in level 1, and geometrical optimization employing Powell's one-direction search method which menimizes only objictive function in level 2. The results of this study acquired by beenning applied to structural model of the truss are as follows : 1. It is verified that the algorithm of this study effectively converges, independent of the initial geometry of the truss and the applied various constraints. 2. The optimum goemetry of the truss varies more considerably according to the constraints selected. 3. Under the condition of the same design, the weight of the truss can be decreased more considerably by means of optimizing even the geometry of truss than by means of optimizing the section of truss while fixing geometrical configuration of it, even though there might be a little difference according to the initial geometry of the truss and the design condition.

• Tunnel and Underground Space
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• v.14 no.1
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• pp.54-68
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• 2004

In this study, scaled model tests were performed on blasting demolition of reinforced concrete structures and the experimental results were analyzed in comparison with the results of numerical analysis. The tests were designed to induce a progressive collapse, and physical properties of the scaled model were determined using scale factors obtained ken dimension analysis. The scaled model structure was made of a mixture of plaster, sand and water at the ratio determined to yield the best scaled-down strength. Lead wire was used as a substitute for reinforcing bars. The scaled length was at the ratio of 1/10. Selecting the material and scaled factors was aimed at obtaining appropriately scaled-down strength. PFC2D (Particle Flow Code 2-Dimension) employing DEM (Distinct Element Method) was used for the numerical analysis. Blasting demolition of scaled 3-D plain concrete laymen structure was filmed and compared to results of numerical simulation. Despite the limits of 2-D simulation the resulting demolition behaviors were similar to each other. Based on the above experimental results in combination with bending test results of RC beam, numerical analysis was carried out to determine the blasting sequence and delay times. Scaled model test of RC structure resulted in remarkably similar collapse with the numerical results up to 900㎳ (mili-second).

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.3
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• pp.181-192
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• 2022

Active vibration control system(AVCS) for helicopter enables to control the vibration generated from the main rotor and has the superb vibration reduction performance with low weight compared passive vibration reduction device. In this paper, FxLMS algorithm-based vibration control software of the light civil helicopter tansmits the control command calculated using the signals of the tachometer and accelerometers to the circular force generator(CFG) is developed and verified. According to the RTCA DO-178C/DO-331, the vibration control software is developed through the model based design technique, and real-time operation performance is evaluated in PILS(processor in-the loop simulation) and HILS(hardware in-the loop simulation) environments. In particular, the reliability of the software is improved through the LDRA-based verification coverage in the PIL environments. In order to AVCS to light civil helicopter(LCH), the dynamic response characteristic model is obtained through the ground/flight tests. AVCS configuration which exhibits the optimal performance is determined using system optimization analysis and flight test and obtain STC certification.

• International Journal of Highway Engineering
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• v.11 no.4
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• pp.69-78
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• 2009

Korea has achieved significant economic growth with building the Gyeongbu Expressway. As the number of new road construction projects has decreased, it becomes more important to maintain optimal status of the current road networks. One of the best ways to accomplish it is weight enforcement as active control measure of traffic load. This study is to develop High-speed Weigh-in-motion System in order to enhance efficiency of weight enforcement, and to analyze patterns of overloaded trucks on highways through the system. Furthermore, it is to review possibilities of developing overweight control system with application of the HS-WIM system. The HS-WIM system developed by this study consists of two sets of an axle load sensor, a loop sensor and a wandering sensor on each lane. A wandering sensor detects whether a travelling vehicle is off the lane or not with the function of checking the location of tire imprint. The sensor of the WIM system has better function of classifying types of vehicles than other existing systems by detecting wheel distance and tire type such as single or dual tire. As a result, its measurement errors regarding 12 types of vehicle classification are very low, which is an advantage of the sensor. The verification tests of the system under all conditions showed that the mean measurement errors of axle weight and gross axle weight were within 15 percent and 7 percent respectively. According to the WIM rate standard of the COST-323, the WIM system of this study is ranked at B(10). It means the system is appropriate for the purpose of design, maintenance and valuation of road infrastructure. The WIM system in testing a 5-axle cargo truck, the most frequently overloaded vehicle among 12 types of vehicles, is ranked at A(5) which means the system is available to control overloaded vehicles. In this case, the measurement errors of axle load and gross axle load were within 8 percent and 5 percent respectively. Weight analysis of all types of vehicles on highways showed that the most frequently overloaded vehicles were type 5, 6, 7 and 12 among 12 vehicle types. As a result, it is necessary to use more effective overweight enforcement system for vehicles which are seriously overloaded due to their lift axles. Traffic volume data depending upon vehicle types is basic information for road design and construction, maintenance, analysis of traffic flow, road policies as well as research.

• Proceedings of the Korean Vacuum Society Conference
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• 2012.08a
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• pp.259-260
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• 2012

산업화가 발달됨에 따라 대기 오염 물질은 점차 증가하고 있는 추세에 있고 특히 기름 및 석탄 연소 보일러, 자동차, 제철, 시멘트 플렌트, 소각로 등은 미세 분진을 발생시키는 주원인이 되어 왔다. 최근 대기환경법은 오염 분진의 중량 규제로부터 $10{\mu}m$ 미만의 PM10에서 $2.5{\mu}m$ 미만의 PM2.5의 미세 분진에 대한 규제로 점차 심화되고 있으나, 이러한 미세분진은 고전적인 제거 방법으로는 매우 어려우며 고가의 HEPA 필터를 사용하여야 한다. 한편 코로나 방전을 이용하는 전기 집진은 미세 먼지 제거에 매우 효율적이어서 $1{\mu}m$ 미만의 미세 분지도 99%까지 제거가 가능하다는 장점이 있지만 입자크기가 클 경우에는 효율이 떨어지는 단점이 있다. 한편 사이클론 집진기는 매우 오래전부터 개발되어 사용되어 왔는데 가격이 저렴하고 운영비가 적게 들며 $10{\mu}m$ 이상의 먼지는 99% 이상 제거가 가능하여 산업현장에서 오랜 기간 사용되어 왔지만 입자크기가 $10{\mu}m$ 미만으로 가면 집진율이 급격히 떨어지는 단점을 가지고 있다. 본 연구에서는 기존의 사이클론 집진기의 구조를 기본으로하여 사이클론 집진기 내부에 플라즈마 방전을 설치하여 원심력에 의한 집진과 코로나 방전에 의한 전기 집진을 동시에 수행할 수 있도록 하이브리드 사이클론 집진기를 제작하였다. 제작된 사이클론 집진기는 직경 30 cm 높이 120 cm의 사이클론 구조를 가지고 있으며 1 hp의 터보송풍기를 장착하여 $20m^3$/min 이상의 유량을 처리할 수 있도록 설계 제작되었다. 제작된 하이브리드 사이클론 집진기의 성능을 평가하기 위하여 $10m^3$의 체적을 가지는 테스트 챔버 내부에 사이클론 집진기를 설치하고 향을 태워 미세 먼지를 발생시킨 후 다양한 조건에서 집진 성능을 측정하여 보았다. 미세 먼지의 경우 사이클론을 작동시키지 않아도 테스트 챔버 벽면에 흡착되어 초기에는 급격히 감소하는 경향을 보여주나 일정 시간이 경과한 후에는 매우 느리게 감소하는 현상이 관찰 되었다. 코로나 방전을 하지 않고 오존 파괴기에 활성탄만 충진한 상태에서 사이크론을 작동시킬 경우 지속적으로 천천히 감소하는 경향을 보여주었으며, 코로나 플라즈마를 방전시킨 경우 미세 먼지는 HEPA filter를 장착한 것보다도 조금 빠르게 미세먼지를 제거하였다. 챔버 내부의 미세먼지가 초기 값의 1/10에 도달하는 시간은 코로나 방전 전류가 증가할수록 짧아지는 경향을 보여주었으며 최적 조건에서 100초 이내에 90% 이상 제거가 가능하였다. 하이브리드 사이클론 집진기는 집진 뿐 만 아리라 VOC 성분도 분해가 가능하여 유해물질을 제거하는 능력이 있다. 유해 가스 제거 능력을 실험하기 위하여 분진제거 실험에 사용된 챔버 안에 아세톤을 증발시켜 50 ppm이 되도록 한 후 다양한 조건에서 유해물질 제거 실험을 수행하였다. 미세먼지와는 달리 장비를 작동하지 않을 경우 매우 느리게 아세톤 농도가 감소하였다. 이는 미세 먼지와는 달리 흡착이 발생하지 않고, 측정 챔버 자체가 완전한 밀폐가 이루어지지 않아 자연적으로 조금씩 외부로 누출되기 때문으로 판단된다. 코로나 플라즈마만 방전시켰을 경우 초기 농도의 80%가 제거되는데 걸리는 시간은 약 28분 정도로 코로나 플라즈마가 VOC 제거에 효과가 있음은 확인하였으나 제거율이 그리 높지 않음을 알 수 있었다. 한편 오존 파괴를 위해 활성탄으로 충진 된 오존파괴기를 통과시킨 경우는 약 12분 경과 후 80%가 제거됨을 확인할 수 있었으나 그 이후에는 VOC의 감소가 매우 느리게 진행됨을 알 수 있었다. 한편 활성탄 대신 $MnO_2$ 복합촉매로 충진 된 오존파괴기를 통과한 경우 약 3분 정도 경과 후 80%의 아세톤이 제거됨을 관찰할 수 있었으며 코로나 플라즈마를 작동시키면서 $MnO_2$ 복합촉매로 충진 된 오존파괴기를 통과시킨 경우 약 2분 정도 경과 80% 이상의 아세톤이 제거되어 코로나 플라즈마와 복합촉매를 사용할 경우 VOC 성분이 효과적으로 제거됨을 알 수 있었다.

• Explosives and Blasting
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• v.22 no.1
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• pp.33-43
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• 2004

In this study, a comparison was made between the resulting behaviors of scaled model test and particle flow analysis for blasting demolition of a reinforced concrete structure. For the test and analysis, a progressive failure of a five-story structure was considered. The dimension analysis was carried out to properly scale down the real structure into the laboratory size. The test model was made of the mixture of gypsum, sand and water along with soldering lead to analogy reinforcing steel bars. The ratio of mixing components was chosen to best represent the scaled down strength and deformation modulus. The columns and girders of the structure were precasted in the laboratory and assembled right before the blasting test. The numerical analysis of the blasting demolition was carried out using PFC2D (Particle Flow Analysis 2-Dimension by Itasca). The results of the blasting of concrete lahmen structure showed roughly identical demolition behavior between scaled model test and numerical test. For the blasting of the reinforced concrete structure, the results were more identical and closer to the real demolition behavior, since the demolition behavior was better represented in this case due to the increased tensile strength of the component.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.16 no.6 s.111
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• pp.665-673
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• 2006

This paper proposes a RSM-based hybrid evolutionary Algorithm (RHEA) which combines the merits of the popular programs such as genetic algorithm (GA), tabu search method and response surface methodology (RSM). This algorithm, for improving the convergent speed that is thought to be the demerit of genetic algorithm, uses response surface methodology and simplex method. The mutation of GA offers random variety to finding the optimum solution. In this study, however, systematic variety can be secured through the use of tabu list. Efficiency of this method has been proven by applying traditional left functions and comparing the results to GA. It was also proved that the newly suggested algorithm is very effective to find the global optimum solution to minimize the weight for avoiding the resonance of fresh water tank that is placed in the after body area of ship. According to the study, GA's convergent speed in initial stages is improved by using RSM method. An optimized solution is calculated without the evaluation of additional actual objective function. In a summary, it is concluded that RHEA is a very powerful global optimization algorithm from the view point of convergent speed and global search ability.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.9
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• pp.175-181
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• 2019

In the case of a conventional single stage decompression regulator used for large depressurization in the hydrogen fuel cell system of a fuel cell electric vehicle (FCEV), problems can arise, such as pulsation, slow response, hydrogen brittleness, leakage, high weight, and high cost due to high decompression. Most of these problems can be overcome easily using two decompression mechanisms (two-stage structures). In addition, a wide outlet-pressure control range can be secured if an electronic solenoid is applied to the second decompression. Accordingly, it is necessary to improve the precision of the outlet pressure of a two-stage pressure-reducing regulator and develop techniques, such as leakage prevention, durability, light weight, and price reduction. Therefore, to improve the outlet pressure accuracy and prevent leakage, the structural part before and after decompression to improve the air tightness were divided and the analysis was carried out assuming that the valve part was closed (open ratio: 0%) after each initial internal pressure application.