• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2857-2861
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• 2007

Flow and aerodynamic characteristics were analyzed numerically for a commercial passenger airplane, Boeing 747-400, flying in the cruising condition. The model geometry with 100:1 in scale was obtained by the photo scanning measurement with the maximum error of 1.4% comparing with the real airplane dimension. The three-dimensional inviscid steady compressible governing equations were solved by the finite volume method in the unstructured grid system. The convective terms were treated by the Crank-Nicholson and first-order upwind schemes. In the computational results, the strong wing-tip vortices were clearly observed and the pressure contours on the airplane surface were suggested. The lift and drag forces in the wing with engines increase by 1.49% and 3.9%, respectively compared with the case without engines. The aerodynamic forces were estimated quantitatively for each element which consists of the airplane.

• 한국경제지리학회지
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• 제11권3호
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• pp.459-475
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• 2008

본 연구의 목적은 최근 다양한 네트워크 분석에 활발히 적용되고 있는 복잡성 분석을 통하여 수도권 지하철 망의 구조적 특성을 연구하는 것이다. 이를 위하여 수도권 지하철 망을 점과 선으로 구성되는 네트워크로 구성하고, 네트워크의 복잡성 분석에서 계산하는 다양 지표들을 산출하여 그에 대한 해석을 시도하였다. 특히 본 연구에서는 교통카드를 이용해 움직이는 수도권 대중교통이용자의 통행기록을 담고 있는 대용량 교통카드 트랜잭션 데이터베이스로부터 수도권 지하철망의 구조적 특징을 찾아내기 위한 알고리즘을 개발하고 그의 적용으로 얻어진 결과를 분석하였다. 또한 지하철역과 역 사이의 시간거리와 실제거리에 대해 최단경로를 탐사하는 알고리즘을 개발하고, 이를 통하여 얻어진 최단경로거리와 최단거리의 분포 구조를 분석하였다. 특히 최단 경로거리와 최단 거리의 합을 산출하여 수도권 지하절망을 통하여 각 역에서 다른 모든 역들에 도달하기 용이한 정도를 의미하는 접근성 지표로 삼고, 이를 GIS를 사용하여 수도권의 접근성의 공간적 분포를 나타내고 그의 공간적 구조를 분석하였다.

• 한국자동차공학회논문집
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• 제18권5호
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• pp.115-123
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• 2010

Cool-down performance after soaking is important because it affects passenger's thermal comfort. The cooling capacity of HVAC system determines initial cool down performance in most cases, the performance is also affected by location, and shape of panel vent, indoor seat arrangement. Therefore, optimal indoor designs are required in developing a new car. In this paper, initial cool down performance is predicted by CFD(computational fluid dynamics) analysis. Experimental time-averaging temperature data are used as inlet boundary condition. For more reliable analysis, real vehicle model and human FE model are used in grid generation procedure. Thermal and aerodynamic characteristics on re-circulation cool vent mode are investigated using CFX 12.0. Thermal comfort represented by PMV(predicted mean vote) is evaluated using acquired numerical data. Temperature and velocity fields show that flow in passenger's compartment after soaking is considerably unstable at the view point of thermodynamics. Volume-averaged temperature is decreased exponentially during overall cool down process. However, temperature monitored at different 16 spots in CFX-Solver shows local variation in head, chest, knee, foot. The cooling speed at the head and chest nearby panel vent are relatively faster than at the knee and foot. Horizontal temperature contour shows asymmetric distribution because of the location of exhaust vent. By evaluating the passenger's thermal comfort, slowest cooling region is found at the driver's seat.

• 한국가시화정보학회지
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• 제5권2호
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• pp.20-25
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• 2007

The geometry of a commercial passenger airplane is realized based on a Boeing 747-400 model through the photographic scanning and reverse engineering. The each element consisting of the plane such as fuselage, wing, vertical fin, stabilizer and engines, is individually generated and then the whole body is assembled by the photomodeler. The maximum error in the realized airplane is about 1.4% comparing with the real one. The three-dimensional inviscid steady compressible governing equations are solved in the unstructured tetrahedron grid system, and in a finite volume method using STAR-CD when the airplane flies at the cruise condition. The pressure distribution on the surface and the wing-tip vortices are visualized, and in addition to the aerodynamics coefficients, lift and drag are estimated.