• Steel and Composite Structures
• /
• 제35권4호
• /
• pp.599-609
• /
• 2020

The tension-only braced frames (TOBFs) are widely used as a lateral force resisting system (LFRS) in low-rise steel buildings due to their simplicity and economic advantage. However, the system has poor seismic energy dissipation capacity and pinched hysteresis behavior caused by early buckling of slender bracing members. The main concern in utilizing the TOBF system is the determination of appropriate performance factors for seismic design. A formalized approach to quantify the seismic performance factor (SPF) based on determining an acceptable margin of safety against collapse is introduced by FEMA P695. The methodology is applied in this paper to assess the SPFs of the TOBF systems. For this purpose, a trial value of the R factor was first employed to design and model a set of TOBF archetype structures. Afterwards, the level of safety against collapse provided by the assumed R factor was investigated by using the non-linear analysis procedure of FEMA P695 comprising incremental dynamic analysis (IDA) under a set of prescribed ground motions. It was found that the R factor of 3.0 is appropriate for safe design of TOBFs. Also, the system overstrength factor (Ω₀) was estimated as 2.0 by performing non-linear static analyses.

• 한국음향학회지
• /
• 제24권4호
• /
• pp.210-216
• /
• 2005

본 논문에서는 잡음에 강인한 음성인식을 위하여 고유공간에 기반을 둔 새로운 특징 정규화 기법을 제안한다. 일반적으로 평균과 분산의 정규화 (MVN)는 켑스트럼 상에서 수행된다. 그러나 최근에 고유공간을 이용한 MVN기법이 소개되었고, 그 고유공간 정규화 기법에서는 하나의 고유공간을 이용하였다. 이 과정에는 켑스트럼 상의 특징 벡터를 선형 주성분 분석 (PCA)행렬을 통하여 고유공간으로 변환시킨 후 MVN을 수행하는 과정이 포함된다. 이 방법에서는 전체 39차의 특징분포를 하나의 고유공간으로 표현하였다. 그러나 이 기법의 경우 전체 특징 분포를 표현함에 세밀함이 떨어지기 때문에 더욱 세밀한 분포의 표현을 위해 본 논문에서는 static 특징, 1차 미분 계수, 2차 미분계수에 각각 유일하고 독립적인 분리된 고유공간을 적용하는 것을 제안하였다. 또한 고유공간에서 정규화 된 훈련 데이터를 이용하여 모델을 만든다. 마지막으로 훈련 데이터의 분포와 잡음환경에서의 테스트 데이터의 분포 특성의 차이를 줄이기 위해 켑스트럼 상에서의 회전 기법을 적용시킨다. 그 결과, 기본적인 고유공간 정규화 기법보다 향상된 성능을 얻을 수 있었다.

• 한국항만경제학회지
• /
• 제30권2호
• /
• pp.93-112
• /
• 2014

한국 해운 물류기업의 경영성과를 연구하기 위해 2012년 매출액이 높은 해운기업 10개, 물류기업10개를 대상으로 2005년부터 2012년까지 재무실적을 기준으로 기업별 성과를 알아보고 사업구조에 따라 4개 유형으로 구분하였다. DEA 활용한 성과측정을 위해 투입요소는 비유동자산과 인건비로, 산출요소는 매출액과 순이익으로 설정하고 CCR, BCC 효율성 분석과 재무실적을 기준으로 성장성과 수익성을 연구하였다. 분석 결과, 효율성과 성장성과수익성을 전체적으로 보면 물류기업의 경영성과가 해운기업보다 높게 나타났고 대기업계열 물류기업의 성과가 물류전문 기업보다 상대적으로 높았다. 정기선 해운기업과 부정기선 해운기업의 최근 성과는 해운시황의 악화 등에 의해 부진한 것으로 나타났다. 세부적으로 보면 대형 화주를 안정적으로 확보하고 장기간 계약구조를 유지하고 있는 기업의 효율성이 높은 것으로 나타났고, 성장성을 보면 다수의 기업에서 비유동자산과 인건비, 매출액이 꾸준하게 증가하고 있는 반면 수익성에서는 대기업계열, 물류전문기업의 수익은 흑자구조를 보이고 있지만, 해운기업의 경우 2008년까지는 물류기업보다 수익성이 높았지만 2009년 이후 많이 악화된 것으로 나타났다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
• /
• pp.128-134
• /
• 2007

본 논문은 고압 축소형 액체로켓엔진 연소기의 연소 성능과 특성에 관한 것이다. 4개의 고압 축소형 연소기 모델에 대하여 연소시험을 수행하였다. 고압 축소형 연소기는 크게 분사기 헤드부, 재생냉각 방식의 연소실부, 그리고 강제 물냉각 노즐부로 구성되어 있고, 1개의 모델은 연소실을 냉각한 연료가 헤드부로 유입되는 재생냉각 방식의 연소기이다. 연소압력은 70 bar이며 재생냉각 방식의 연소기 모델은 연소시험 중 고주파 연소불안정이 발생하여 하드웨어가 손상되었다. 각각의 고압 축소형 연소기의 연소시험 결과, 성능 비교 및 정압, 동압 특성에 대해 기술하였다.

• Structural Engineering and Mechanics
• /
• 제13권5호
• /
• pp.557-568
• /
• 2002

For the evaluation of the capability of a tubular member of an offshore structure to absorb the collision energy, a simple method can be employed for the collision analysis without performing the detailed analysis. The most common simple method is the rigid-plastic method. However, in this method any characteristics for horizontal movement and rotation at the ends of the corresponding tubular member are not included. In a real structural system of an offshore structure, tubular members sustain a certain degree of elastic support from the adjacent structure. End fixity has influences in the behaviors of a tubular member. Three-dimensional FEM analysis can include the effect of end fixity fully, however in viewpoints of the inherent computational complexities of the 3-D approach, this is not the recommendable analysis at the initial design stage. In this paper, influence of end fixity on the behaviors of a tubular member is investigated, through a new approach and other approaches. A new analysis approach that includes the flexibility of the boundary points of the member is developed here. The flexibility at the ends of a tubular element is extracted using the rational reduction of the modeling characteristics. The property reduction is based on the static condensation of the related global stiffness matrix of a model to end nodal points of the tubular element. The load-displacement relation at the collision point of the tubular member with and without the end flexibility is obtained and compared. The new method lies between the rigid-plastic method and the 3-demensional analysis. It is self-evident that the rigid-plastic method gives high strengthening membrane effect of the member during global deformation, resulting in a steeper slope than the present method. On the while, full 3-D analysis gives less strengthening membrane effect on the member, resulting in a slow going load-displacement curve. Comparison of the load-displacement curves by the new approach with those by conventional methods gives the figures of the influence of end fixity on post-yielding behaviors of the relevant tubular member. One of the main contributions of this investigation is the development of an analytical rational procedure to figure out the post-yielding behaviors of a tubular member in offshore structures.

• 한국추진공학회지
• /
• 제18권3호
• /
• pp.70-77
• /
• 2014

본 논문은 한국형 2.75 인치 로켓 추진기관의 독자 모델 개발에 관하여 기술하였다. 개발된 한국형 2.75 인치 로켓 추진기관은 추진제 그레인의 형상변경을 통하여 화염안정성을 증대시켰으며, 점화장치에 EMI 필터를 장착하여 우발점화 방지기능을 추가하였다. 그리고 노즐 형상 변경 및 날개 수 증가를 통하여 비행안정성의 향상을 가질 수 있었다. 지상연소시험 및 온도충격시험을 통해 추진제의 성능을 검증하였으며, 약 210 발의 비행시험을 통해 기 배치된 추진기관과 비행성능이 동일함을 입증하였다. 성능개량과 더불어 한국형 독자모델 개발로 인한 지적재산권 문제 극복에 기여할 수 있는 근간을 마련했다는데 그 의의가 있다.

• Structural Engineering and Mechanics
• /
• 제31권5호
• /
• pp.507-526
• /
• 2009

Based on numerical and experimental methods, a systematic structural evaluation of a steel natatorium in service was carried out in detail in this paper. Planning of inspection tasks was proposed firstly according to some national codes in China in order to obtain the economic and reliable results. The field visual inspections and static computation were conducted in turn under in-service environmental conditions. Further a three-dimensional finite element model was developed according to its factual geometry properties obtained from the field inspection. An analytical modal analysis was performed to provide the analytical modal properties. The field vibration tests on the natatorium were conducted and then two different system identification methods were used to obtain the dynamic characteristics of the natatorium. A good correlation was achieved in results obtained from the two system identification methods and the finite element method (FEM). The numerical and experimental results demonstrated that the main structure of the natatorium in its present status is safe and it still satisfies the demand of the national codes in China. But the roof system such as purlines and skeletons must be removed and rebuilt completely. Moreover the system identification results showed that field vibration test is sufficient to identify the reliable dynamic properties of the natatorium. The constructive suggestion on structural evaluation of the natatorium is that periodic assessment work must be maintained to ensure the natatorium's safety in the future.

• 설비공학논문집
• /
• 제17권4호
• /
• pp.386-395
• /
• 2005

With the development of a living standard, the importance of indoor air conditioning system in all kinds of buildings and vehicles has increased. A lot of researches on energy losses in a duct and various kinds of flow pattern in branches or junctions have been carried out over many years, because the primary object of a duct system used in HVAC is to provide equal flow rate in the interior of each room by minimizing pressure drop. In this study, to get equal flow distribution in each branch, a blockage is applied to the rectangular duct system. The flow analysis for flow distribution of a rectangular duct with two branches was performed by CFD. By using SIMPLE algorithm and finite volume method, flow analysis is performed in the case of 3-D, incompressible, turbulent flow. Also, the standard $k-{\varepsilon}$ model and wall function method were used for analysis of turbulent fluid flow. The distribution diagrams of static pressure, velocity vector, turbulent energy and kinetic energy in accordance with variation of Reynolds number and blockages location in a rectangular duct show that flow distribution at duct outlets is improved by a blockage. In this rectangular duct system, mean velocity and flow rate distribution in two branch outlets are nearly constant regardless of variation of Reynolds number, and a flow pattern of the internal duct has a same tendency as well.

• 한국철도학회:학술대회논문집
• /
• 한국철도학회 2008년도 춘계학술대회 논문집
• /
• pp.1903-1908
• /
• 2008

This paper presents a characteristics of linear induction motor considering airgap variation for railway transit in order to achieve high performance of the vehicle. The operating principle of a LIM(Linear induction motor) is identical to a rotary induction motor. Space-time variant magnetic fields are generated by the primary part across the airgap and induce the electro-motive force(EMF) in the secondary part, a conducting sheet. This EMF generates the eddy currents, which interact with the airgap flux and so produce the thrust force known as Loren's force. Even though the operating principal is exactly same as a rotary motor, the linear motor has a finite length of the primary or secondary parts and it causes static and dynamic end-effect which is the discontinuous airgap flux phenomenon. This end-effect causes the deterioration of the system performance, especially in high-speed operation. Another problem is that construction tolerance restricts the minimum airgap in order to prevent a collision between the primary part and the secondary reaction plate. More over, as the airgap length is getting smaller, the attraction force between the primary part and secondary parts is getting larger dramatically and the attraction force would be another friction against propulsion. Therefore, it is necessary to figure out the characteristics of linear induction motor considering airgap variation in order to achieve high performance of the vehicle. The dynamic model of LIM taking into account end-effects is derived. Then the modified mechanical load equation considering the effect of the attraction and thrust force according to the airgap variation is analyzed. The simulation results are presented to show the effect of the LIM according to the airgap variation.

• 한국전산구조공학회논문집
• /
• 제25권3호
• /
• pp.259-266
• /
• 2012

본 논문에서는 벽식 구조시스템의 일부 전단벽을 제거하여 공간의 가변성을 높인 무량복합 구조시스템의 내진성능을 ATC-63에 제시되어 있는 절차에 따라 파악하였으며, 동일한 규모의 벽식 구조시스템의 내진성능과 비교하였다. 해석모델로 12층 무량복합 및 벽식 구조시스템을 KBC 2009에 따라 설계하고 비선형 정적 및 비선형 증분 동적해석(IDA)을 수행하여 지진응답 및 붕괴거동을 파악하였다. 무량복합 시스템은 벽식 구조시스템 보다 적은 양의 콘크리트 물량으로 설계되었으며, 동일한 지진하중에 대하여 좀 더 큰 변위응답을 보이는 것으로 나타났다. IDA 해석결과 얻어진 붕괴 여유비(CMR)는 ATC-63에 제시된 한계상태를 만족하여 설계지진하중에 대하여 충분한 내진성능을 보유한 것으로 나타났다.