Earticle

소프트웨어 프로젝트를 개발하는 방법론에는 20여 가지의 개발 프로세스 모델들이 존재한다. 그러나 모든 소프트웨어의 특성을 만족시킬 수 있는 일반화된 하나의 모델이 없는 실정으로 개발조직은 여러 모델들을 적절히 혼합하여 개발될 시스템과 개발팀의 능력에 맞도록 새로운 모델을 개발하여야만 한다. 본 논문에서는 다양한 소프트웨어 개발 상황에 보다 적합할 것으로 판단되는 동시개발 프로세스 모델을 제안한다. 먼저, 개발 요구사항 목록들이 작성되면, 요구사항을 중요도에 따라 20:80 비율로 분할하고, 중요한 20% 요구사항의 요구사항 분석과 아키텍쳐 설계가 완료될 때까지는 순차적으로 수행한다. 20%의 중요 요구사항에 대해 상세설계를 시작하는 시점에서 나머지 80%의 요구사항에 대한 요구사항 분석단계를 동시에 수행하는 개념이다. 동시개발은 타임박스(Timebox) 개념으로 수행되며, 이때 적용되는 순차적, 반복적 & 점진적 또는 Agile 방법들에 따라 각 타임박스에서 개발되는 요구사항의 분할 비율은 차이가 발생한다. 순차적, 반복적 & 점진적 또는 Agile 방법론을 동시개발 개념을 적용한 결과 단일화된 프로세스 모델로 표현할 수 있었다. 제안된 모델은 개발 단계들을 팀 단위로 수행할 경우 개발자원 활용의 비효율성을 크게 줄일 수 있다. 또한, 동시개발 개념을 적용하여 단계들이 중첩되어 수행되므로 개발기간도 크게 단축시키는 장점이 있다. 따라서 제안된 모델은 보다 빠른 시간에 보다 저렴한 비용으로 보다 좋은 품질의 소프트웨어를 개발하여 고객에게 납품할 수 있어 고객을 만족도를 향상시킬 수 있으며, 더불어 소프트웨어 개발 성공률을 높이는데도 기여할 것으로 판단된다.

Though a dozen of different software life cycle models are suggested, there is no universal model which can satisfy all the characteristics of software. Organizations mix and match different life cycle models to develop a model more tailored for their systems and capabilities. We suggest overlapped-concurrent development life cycle model that is more suitable in various software development environment. Firstly, we divided the development process into abstract and implementation stage. Abstract stage is from software concept phase to detailed design starting time, and implementation stage is from detailed design phase to system testing phase. Next, the abstract stage introduced the overlapped phase concept that begins the next phase when the step is completed 20% by applying pareto's law. In the implementation stage, we introduced the concurrent development which the several phases are performed some time as when one use-case (UC) is completed the next development phase is started immediately. The proposed model has an advantage that it can reduce the inefficiency of development resource greatly. This model can increase the customer satisfaction with a great product at a low cost and on a short schedule. Also, this model can contribute to increase the software development success rate.

다단임팩터(cascade impactor)는 대기환경 연구에 있어 입자상물질의 물리 화학적 분석에 유용하게 사용되고 있는 입자상물질 포집장치이다. 다단임팩터의 각 단은 외벽(stage wall), 가속노즐판(acceleration nozzle plate)과 충돌판(impaction plate)으로 구성되며 충돌판에는 입자상물질의 포집을 위하여 테플론 필터, 알루미늄 필터 등을 장착하게 되어 있다. (중략)

An efficient time-domain numerical method for the analysis of broadband noise generation and propagation due to turbulence-cascade interaction is developed. The core algorithm of the present method is based on the B-periodicity of the acoustic response function of the flat-airfoil cascade to the ingesting gust (B denotes the number of airfoils in the cascade). To confirm this periodicity, gust-cascade interaction problem are solved by using the time-domain method, which shows that the incident gust with the circumferential mode number having the same remainders when divided by the airfoil number excites the same acoustic response of the cascade. Using the proposed fast algorithm with this periodicity, we show that the total computation time for the model broadband problem using the total 525 incident gust modes can be reduced to about 1/4 of that taken in using the previous time-domain program.

It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study(1) showed that Perfectly Matched Layer (PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.

In this paper, we propose a smart transformer for a smart transformer miniature model, which can replace a 60 [Hz] single-phase transformer installed in an electric vehicle. The proposed smart transformer is lighter than a conventional transformer, can control instantaneous voltage, and can be expected to improve power quality through harmonic compensation. The proposed intelligent transformer consists of an incoming part, an AC/DC converter, and a dual active bridge. Only the incoming part and the AC/DC converter are described in this paper. The proposed intelligent transformer has 75 kVA 3.3 kV input and 750 V DC output, which are verified by simulation and experiment.