• Computational Structural Engineering
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• v.3 no.2
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• pp.9-12
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• 1990

유한요소법은 구조물의 변위 또는 응력 등을 해석하기 위한 구조해석 분야에서 뿐만 아니라, 유체역학, 열역학 및 전자기학 등 각종 공학문제의 수학적 모형에 대하여 구해진 미분방정식을 푸는 기법으로 널리 사용되고 있다. 특히, 컴퓨터 기술의 급속한 발달로 인한 유한요소법의 적용범위는 더욱 확장되고 있다. 본 고는 유한요소법이 타 공학문제, 특히 유체에 관련된 문제에서 어떻게 이용되고 있는가를 소개하려 한다. 구체적으로, 해양구조물의 설계에 있어서 선결되어야 할 주요사항인 파랑하중 산정문제를 예로 들어, 유한요소법을 이용한 이의 수식화과정을 간략히 설명하였다.

• 한국전산유체공학회:학술대회논문집
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• 2010.05a
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• pp.78-82
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• 2010

An integrated multi-disciplinary design system plays a critical role in the preliminary design of an aircraft. In this paper such system is developed for the multi-disciplinary computation and design; aerodynamics elasticity, and radio frequency stealth. Common data base of geometry and structured grids is generated and used for aerodynamic, structural and eletromagnetics analysis. The Navier-Stokes CFD, FEM, and CEM technique are used for aerodynamic, structural, and RF stealth computations respectively.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.4
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• pp.1-6
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• 2005

The ability to predict radar return from flying vehicles becomes a critical technology issue in the development of stealth configurations. Toward developing a CEM code based on Maxwell's equations for analysis of RCS reduction schemes, an explicit upwind scheme suitable for multidisciplinary design is presented. The DFFT algorithm is utilized to convert the time-domain field values to the frequency-domain. A Green's function based on near field-to-far field transformation is also employed to calculate the bistatic RCS. To verify the numerical calculation the two-dimensional field around a perfectly conducting cylinder is considered. Finally results are obtained for the scattering electromagnetic field around an airfoil in order to illustrate the feasibility of applying CFD based methods to CEM.