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박영민,정진덕,Park, Youngmin,Chung, Jindeog 항공우주시스템공학회 2015 항공우주시스템공학회지 Vol.9 No.4
During the conceptual design of turboprop aircraft, the power effect driven from rotating propeller is typically obtained from empirical data. In the present paper, propeller power effect was obtained by using unsteady three-dimensional Navier-Stokes solver with $k-{\omega}$ turbulence model for the accurate prediction of turboprop aircraft performance. In order to simulate the relative motion between propeller and fuselage, unsteady sliding mesh method was used. During simulation, three flow conditions such as climb, cruise and descending flight were selected considering the flight envelop of the real turboprop aircraft. For the correction of aerodynamic coefficients, the thrust effect of engine exhaust gas was included based on the engine manufacturer's data. Using the computational results, the correction table for the aerodynamic coefficient of turboprop aircraft was suggested for the performance analysis of turboprop aircraft.
박영민,강형민,정진덕,이해창,Park, Youngmin,Kang, Hyoungmin,Chung, Jindeog,Lee, Hae-Chang 항공우주시스템공학회 2013 항공우주시스템공학회지 Vol.7 No.3
Numerical optimization of two dimensional high lift configuration was performed with flow solver and optimization method based on RSM(Response Surface Model). Navier-Stokes solver with Spalart-Allmaras turbulence model was selected for the simulation of highly complex and separated flows on the flap. For the simultaneous optimization of both flap shape and setting (gap/overlap), 10 design variables (eight variables for flap shape variation and two variables for flap setting) were chosen. In order to generate the response surface model, 128 experimental points were selected for 10 design variables. The objective function considering maximum lift coefficient, lift to drag ratio and lift coefficient at specific angle of attack was selected to reduce flow separation on the flap surface. The present method was applied to two dimensional fowler flap in landing configuration. After applying the present method, it was shown that the optimized high lift configuration had less flow separation on the flap surface and lift to drag ratio was suppressed over entire angle of attack range.
디클러스터링된 공간 데이타베이스에서 다중 공간 질의 처리
박영민(Park Youngmin),전봉기(Jun Bonggi),서영덕(Seo Youngdeok),홍봉희(Hong Bonghee) 한국정보과학회 1999 한국정보과학회 학술발표논문집 Vol.26 No.2Ⅰ
다중 공간 질의는 동시에 2개 이상 수행되는 영역 질의로 정의되며 인터넷 기반 지도 보기 응용의 주요 연산이 되므로, 질의 처리 속도의 향상을 위해서 병렬로 처리되어야 하고 디스크 입출력 비용을 최대한 줄일 필요가 있다. 그런데 다중 공간 질의는 디스크 입출력 비용을 개선하기 위해 다중 CPU/다중 디스크 구조 상에서 디클러스터링을 수행하더라도 디스크 임의 탐색이 발생하는 문제점이 있다. 이 논문에서는 디클러스터링된 공간 데이타베이스에서 다중 공간 질의를 처리할 때 발생하는 문제점인 질의 간임의 탐색을 분석하고, 해결 방안으로 질의 간 위치 관련성과 질의 처리 이력을 이용한 질의 스케줄링 기법을 제안하고 구현하였다. 실험을 통한 성능 평가 결과, 질의 스케줄링을 수행할 경우 디스크 입출력 비용을 줄일 수 있어 다중 공간 질의 처리시의 성능을 개선할 수 있는 것으로 나타났다.