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이병준,전홍석,송호영,Lee, B.J.,Jeon, H.S.,Song, H.Y. 한국전자통신연구원 2012 전자통신동향분석 Vol.27 No.2
정보 중심 네트워킹(Information Centric Networking)은 단대단(end-to-end)으로 통신을 수행하는 기존의 인터넷 통신 패러다임을 정보 중심적으로 재편하려는 시도이다. 이 방법론에 따르면, 통신을 원하는 개체는 통신 대상 호스트(host)의 주소를 명시하는 대신, 통신 대상 정보의 식별자(identifier)를 명시하여 통신을 시작한다. 네트워크는 해당 식별자를 통해 어떤 정보를 서비스하여야 하는지 알아낸 뒤 해당 정보를 전송한다. 정보 중심 네트워킹 패러다임을 지지하는 연구자들은 이러한 통신 메커니즘이 기존의 IP 중심적 네트워킹 구조가 갖는 여러 가지 이슈들에 대한 본질적인 해결책이 될 수 있을 것이라 믿는다. 본고에서는 정보 중심 네트워킹에 관한 연구 동향 및 대표적 연구 프로젝트들을 살펴보고, 앞으로 해결되어야 하는 이슈들을 점검한다.
천음속 난류 유동장에서의 다중체 항공기 형상의 공력 설계 도구의 개발
이병준(B.J. Lee),이준석(J.S. Lee),임진우(J.W. Yim),김종암(Chongam Kim) 한국전산유체공학회 2007 한국전산유체공학회 학술대회논문집 Vol.2007 No.-
A new design approach for a delicate treatment of complex geometries such as a wing/body configuration is arranged using overset mesh technique under large scale computing environment for turbulent viscous flow. Various pre- and post-processing techniques which are required of overset flow analysis and sensitivity analysis codes are discussed for design optimization problems based on gradient based optimization method (GBOM). The overset flow analysis code is validated by comparing with the experimental data of a wing/body configuration (DLR-F4) from the 1st Drag Prediction Workshop (DPW-Ⅰ). In order to examine the applicability of the present design tools, careful design works for the drag minimization problem of a wing/body configuration are carried out by using the developed aerodynamic shape optimization tools for the viscous flow over multiple-body aircraft geometries.
이병준(B.J. Lee),김종암(C. Kim) 한국전산유체공학회 2006 한국전산유체공학회지 Vol.11 No.1
An optimal shape design approach is presented for a subsonic S-shaped intake using aerodynamic sensitivity analysis. Two-equation turbulence model is employed to capture strong counter vortices in the S-shaped duct more precisely. Sensitivity analysis is performed for the three-dimensional Navier-Stokes equations coupled with two-equation turbulence models using a discrete adjoint method For code validation, the result of the flow solver is compared with experiment data and other computational results of bench marking test. To study the influence of turbulence models and grid refinement on the duct flow analysis, the results from several turbulence models are compared with one another and the minimum number of grid points, which can yield an accurate solution is investigated The adjoin: variable code is validated by comparing the complex step derivative results. To realize a sufficient and flexible design space, NURBS equations are introduced as a geometric representation and a new grid modification technique, Least Square NURBS Grid Approximation is applied. With the verified flow solver, the sensitivity analysis code and the geometric modification technique, the optimization of S-shaped intake is carried out and the enhancement of overall intake performance is achieved The designed S-shaped duct is tested in several off-design conditions to confirm the robustness of the current design approach. As a result, the capability and the efficiency of the present design tools are successfully demonstrated in three-dimensional highly turbulent internal flow design and off-design conditions.