• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 춘계학술대회논문집
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• pp.638-643
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• 2005

This study is about a semi-active quarter car simulation method including a MR(magneto-rheological) damper. The MR damper was modeled as Spencer model that can capture nonlinear and hysteretic behavior. The parameters of the Spencer model were extracted from a random excitation test and optimum treatment of the test data. Then, a suspension control algorithm based on Sky-hook theory was applied for the quarter car simulation. Also, an experiment was dong using a quarter car simulator to confirm the simulation results with the Spencer MR damper model

• Journal of Computing Science and Engineering
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• 제5권2호
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• pp.150-160
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• 2011

Automatic text classification has a long history and many studies have been conducted in this field. In particular, many machine learning algorithms and information retrieval techniques have been applied to text classification tasks. Even though much technical progress has been made in text classification, there is still room for improvement in text classification. In this paper, we will discuss remaining issues in improving text classification. In this paper, three improvement issues are presented including automatic training data generation, noisy data treatment and term weighting and indexing, and four actual studies and their empirical results for those issues are introduced. First, the semi-supervised learning technique is applied to text classification to efficiently create training data. For effective noisy data treatment, a noisy data reduction method and a robust text classifier from noisy data are developed as a solution. Finally, the term weighting and indexing technique is revised by reflecting the importance of sentences into term weight calculation using summarization techniques.

• 한국소음진동공학회논문집
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• 제15권9호
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• pp.1016-1022
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• 2005

This study is about a semi-active quarter car simulation method including a MR(magneto-rheological) damper. The MR damper was modeled as Spencer model that can capture nonlinear and hysteretic behavior. The parameters of the Spencer model were extracted from a random excitation test and optimum treatment of the test data. Then, a suspension control algorithm based on Sky-hook theory was applied for the quarter car simulation. Also, an experiment was done using a quarter car simulator to confirm the simulation results with the Spencer MR damper model.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1998년도 춘계학술대회논문집
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• pp.179-184
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• 1998

Semi-solid forging can be applied in industry only with enough knowledge of the effects of the forming parameters related with the process and their exact control which can be obtained by empirical or numerical methods. In the current study, the effects of process variables on semi-solid forging are discussed based on mainly numerical results. Die preheating temperature, initial solid fraction of the workpiece, and die velocity were selected as process variables, and numerical analyses using a rigid-thermoviscoplastic finite element approach that considered the release of latent heat due to phase change were carried out. In the analyses, a proposed flow stress material characterization and a solid fraction updating algorithm were employed. The obtained results from numerical analysis are discussed and are compared with some experimental observations.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.29-33
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• 2005

고체 램 제트 추진기관에서도 일반 로켓 추진기관에서와 같이 Isp 즉 추력을 증대 시키기 위하여 고체 입자들을 연료에 함유시킨다. 이러한 고체입자가 포함된 연료들은 매우 짧은 연소실 체류시간 때문에 연소 효율의 증대가 필수적이며 흡입공기 온도가 중요한 역할을 한다. 이 흡입공기 온도가 램 제트 성능에 미치는 영향을 조사하였다 성능조사는 실험적 방법에 한계가 있어 연소실험을 통한 연소효율을 이용하여 반-실험적으로 조사하였다. 연소실 흡입공기 온도에 영향을 미치는 인자는 자유 유동장 즉 대기 온도와 비행 마하 수이며 이들에 대한 효과를 조사하였다.

• Steel and Composite Structures
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• 제28권2호
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• pp.209-221
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• 2018

An empirical and efficient method is presented for calculating the dynamic increase factor to amplify the applied loads on the affected bays of a steel frame structure with semi-rigid connections. The nonlinear static alternate path analysis is used to evaluate the dynamic responses. First, the polynomial models of the extended end plate and the top and seat connection are modified, and the proposed polynomial model of the flush end plate connection shows good agreement as compared with experimental results. Next, a beam model with nonlinear spring elements and plastic hinges is utilized to incorporate the combined effect of connection flexibility and material nonlinearity. A new step-by-step analysis procedure is established to obtain quickly the dynamic increase factor based on a combination of the pushdown analysis and nonlinear dynamic analysis. Finally, the modified dynamic increase factor equation, defined as a function of the maximum ratio value of energy demand to energy capacity of an affected beam, is derived by curve fitting data points generated by the different analysis cases with different column removal scenarios and five types of semi-rigid connections.

• International Journal of Naval Architecture and Ocean Engineering
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• 제13권1호
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• pp.718-733
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• 2021

A prediction method, based on the Morison equation as well as Froude-Krylov formula, is presented to simulate the loads acting on the columns and caissons of the semi-submersible platform induced by Internal Solitary Wave (ISW) respectively. Combined with the experimental results, empirical formulas of the drag and inertia coefficients in Morison equation can be determined as a function of the Keulegan-Carpenter (KC) number, Reynolds number (Re) and upper layer depth h₁/h respectively. The experimental and calculated results are compared. And a good agreement is observed, which proves that the present prediction method can be used for analyzing the ISW-forces on the semi-submersible platform. Moreover, the results also demonstrate the layer thickness ratio has a significant effect upon the maximum horizontal forces on the columns and caissons, but both minimum horizontal and vertical forces are scarcely affected. In addition, the incoming wave directions may also contribute greatly to the values of horizontal forces exerted on the caissons, which can be ignored in the vertical force analysis.

• Journal of Mechanical Science and Technology
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• 제16권8호
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• pp.1144-1153
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• 2002

A hybrid performance prediction method is proposed in the present study. A channel diffuser is divided into four subregions: vaneless space, semi-vaneless space, channel, and channel exit region. One-dimensional compressible core flow and boundary layer calculation of each region with an incidence loss model and empirical correlation of residuary pressure recovery coefficient of a channel predict the performance of diffusers. Three channel diffusers are designed and tested for validating the developed prediction method. The pressure distributions from an impeller exit to the channel diffuser exit are measured and discussed for various operating conditions from choke to nearly surge conditions. The strong non-uniform pressure distribution which is caused by impeller-diffuser interaction is obtained over the vaneless and semi-vaneless spaces. The predicted performance shows good agreement with the measured performance of diffusers at a design condition as well as at off-design conditions.

• 대한화학회지
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• 제26권4호
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• pp.195-204
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• 1982

n-부탄, n-부틸 라디칼, 그리고 테트라메틸렌 디라디칼(3중항)의 여러 기하학적 구조에 관하여 STO-3G 방법으로 얻은 고유값 및 고유함수 성질들을 반경험적인 MO계산으로 얻은 결과와 비교하여 보기 위하여 EHT, CNDO/2, MINDO/3, 그리고 MNDO계산을 수행하였다. 그 결과 n-부탄의 여러 형태에 대한 안정성 순서는 모든 방법에서 같았으며 일전자에너지항에 의존하였고 ${\pi}$-오비탈에너지 변화는 반경험적 계산에서 훨씬 중요함을 알았다. $(n-{\sigma}^{\ast})_{trans}$에서 $(n-{\sigma}{\ast})_{cis}$로 구조가 바뀔때 수반되는 hyperconjugation 에너지 변화는 EHT, CNDO/2, MINDO/3 계산에서 작게 계산된 반면에 MNDO 계산에서는 크게 계산되었다. 주로 $(n-{\sigma}{\ast})_{trans}$의 구조에 수반되는 매우 큰 핵간 반발에너지 때문에 $(n-{\sigma}{\ast})_{trans}$는 알짜 불안정화 효과를 나타내었다. Through-space 상호작용으로 디라디칼의 $n_1$ 및 $n_2$ 오비탈간의 에너지 차이 ${\Delta}E-{sp}$ 및 ${\Delta}{\varepsilon}={\varepsilon}_0$-${\varepsilon}_{av}$를 작게함을 알았다 : through-space 상호작용은 through-bond 상호작용과 반대의 효과를 나타내었다. 비교적 심하지 않은 NDO 근사를 사용한 MNDO법에서는 이러한 에너지 차이가 작아지는 효과가 확대되어 나타났다. 특히 ${\sigma}-{\sigma}{\ast}$ 및 $n-{\sigma}{\ast}$ 상호작용이 수반되는 경우에서는 일반적으로 반경험적 방법으로 계산한 오비탈 성질들은 STO-3G 방법으로 계산한 결과와 만족스럽게 일치 하였으나 고유값에 관여된 성질들은 만족스럽지 못함을 알았다.

• 한국전산유체공학회지
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• 제20권2호
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• pp.16-22
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• 2015

The pressure is generally lower than that of the freestream at the base of a missile body due to the energy loss by the flow separation around the edge of the base. The base pressure changes in the presence of the thrust jet due to the interaction between the base flow of the missile and the jet flow. In this study, behavior of the missile base pressure by the change of the jet exit pressure and the freestream condition is investigated using the CFD(Computational Fluid Dynamics) method. Effects of the grid type and the freestream condition are tested. The results are compared with the semi-empirical predictions and the flight test data. The CFD results agree well with the flight test data. The semi-empirical predictions overestimate the base pressure when jet thrust is strong for low freestream speed.