• Water Engineering Research
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• 제4권1호
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• pp.45-58
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• 2003

Two-dimensional depth-averaged advection-dispersion equation was simulated using FEM. In the straight rectangular channel, the advection-dispersion processes are simulated so that these results can be compared with analyti-cal solutions for the transverse line injection and the point injection. In the straight domain the standard Galerkin method with the linear basis function is found to be inadequate to the advection-dispersion analysis compared to the upwind finite element scheme. The experimental data in the S-curved channel were compared with the result by the numerical model using SUPG(Streamline upwind Petrov-Galerkin) method.

• 대한기계학회논문집
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• 제16권3호
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• pp.419-429
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• 1992

본 연구에서는 면외 변형이 가능한 평면 곡선보에 수정 형상함수를 적용하여 탈락성 및 지속성 에너지에 포함된 가성구속에 의한 수치해의 거동을 고찰함과 동시에, 가성구속에 의한 오차 발생 요인이 제거된, 면외 변형이 가능한 평면 곡선보의 선형 요소를 제안하고자 한다.

• 대한조선학회논문집
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• 제32권4호
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• pp.114-122
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• 1995

본 논문에서는 물질경계면을 갖는 선형탄성체에서의 응력파를 수치적으로 해석하는 기법이 소개되었으며 사각판에 대해 bicharacteristic법을 사용하여 개발된 수치해석법이 곡선경계면을 갖는 판으로 확장되었다. 제안된 개념의 효용성을 검증하기 위하여 수치해석 결과가 이론적으로 잘 알려진 응력파의 물리적 특성을 재현시켜 주는지 검토되었으며 곡선경계면을 갖는 판에 있어서 실험결과와 비교계산이 수행되었다. 또한 곡선 가장자리와 물질경계면에서 반사와 회절에 의한 응력촛점현상에 대해서도 조사되었다.

• Advances in nano research
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• 제7권3호
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• pp.181-190
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• 2019

The thermal buckling temperature values of the graded carbon nanotube reinforced composite shell structure is explored using higher-order mid-plane kinematics and multiscale constituent modeling under two different thermal fields. The critical values of buckling temperature including the effect of in-plane thermal loading are computed numerically by minimizing the final energy expression through a linear isoparametric finite element technique. The governing equation of the multiscale nanocomposite is derived via the variational principle including the geometrical distortion through Green-Lagrange strain. Additionally, the model includes different grading patterns of nanotube through the panel thickness to improve the structural strength. The reliability and accuracy of the developed finite element model are varified by comparison and convergence studies. Finally, the applicability of present developed model was highlight by enlighten several numerical examples for various type shell geometries and design parameters.

• Elastomers and Composites
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• 제55권4호
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• pp.329-338
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• 2020

In this study, three different die geometries were selected to understand the die characteristics in the film casting extrusion processes. First, large and small-scale T-dies were numerically simulated to observe the scaled-down effect on the flow inside the dies. Second, three different dies-keyhole, linear tapper coat-hanger die (LTCD), and curved tapper coat-hanger die (CTCD)-were numerically observed and discussed according to the mass flow rate. Finally, the die exit velocity profiles and die characteristics were observed and discussed based on the power-law index for the LTCD die. These numerical simulations and numerical data will aid the optimization of the die design in industrial fields.

• 천문학회보
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• 제46권2호
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• pp.56.3-56.3
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• 2021

In a ΛCDM universe, most galaxies are believed to evolve by mergers and accretions. The debris resulting from such processes remains faint and/or diffuse structures, such as tidal streams and stellar halos. Although these structures are a good indicator of the recent mass assembly history of galaxies, they have the disadvantage of being difficult to observe due to their low surface brightness (LSB). To recover these LSB features by reducing the photometric uncertainties introduced by the optics system, we attempt to develop an optimized telescope, called a linear astigmatism free-three mirror system, that minimizes the loss and scattering of light within the telescope. With that prototype, we observe NGC 5907, known as a nearby galaxy with a fabulous loop structure(s), to inspect its performance. After a dedicated data reduction process, including flat-fielding with dark sky flat and sky subtraction, our observation reaches a 1σ surface brightness limit of μlim,r ≃ 28.3 mag arcsec-2 in 10×10 arcsec boxes. We finally identify a single tidal stream that is likely the remnant of a nearly disrupted galaxy. This finding emphasizes that the capability of LSB detection with our telescope is comparable to that of much larger telescopes.

• International Journal of Aeronautical and Space Sciences
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• 제15권1호
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• pp.32-43
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• 2014

Automatic fiber placement (AFP) has become a popular processing technique for composites in the aerospace industry, due to its ability to place prepregs or tapes precisely in the exact position when complex parts are being manufactured. This paper presents the design, analysis, and manufacture of an AFP mandrel for composite aircraft fuselage skin fabrication. According to the design requirements, an AFP mandrel was developed and a numerical study was performed through the finite element method. Linear static load analyses were performed considering the mandrel structure self-weight and a 2940 N load from the AFP machine head. Modal analysis was also performed to determine the mandrel's natural frequencies. These analyses confirmed that the proposed mandrel meets the design requirements. A prototype mandrel was then manufactured and used to fabricate a composite fuselage skin. Material load tests were conducted on the AFP fuselage skin curved laminates, equivalent flat AFP, and hand layup laminates. The flat AFP and hand layup laminates showed almost identical strength results in tension and compression. Compared to hand layup, the flat AFP laminate modulus was 5.2% higher in tension and 12.6% lower in compression. The AFP curved laminates had an ultimate compressive strength of 1.6% to 8.7% higher than flat laminates. The FEM simulation predicted strengths were 4% higher in tension and 11% higher in compression than the flat laminate test results.

• 한국터널지하공간학회 논문집
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• 제14권6호
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• pp.595-606
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• 2012

강재의 강지적인 사용으로 인한 부식 등과 같은 문제점을 보완할 수 있는 대체 재료로서, 섬유강화 복합재료의 활용이 증대되고 있다. 하지만 일반적으로 선형의 섬유강화 복합재료를 아치형인 터널구조물의 부재로서 활용하는 데는 많은 문제점이 대두된다. 본 연구에서는 FRP 복합부재의 거동특성 파악을 위해 FRP와 콘크리트 합성부재에 대한 하중재하 실험을 수행하였다. 또한 역학적 거동분석을 위하여 동일 조건에 대한 수치해석을 수행하였다. 하중재하 실험 및 수치해석결과, FRP와 콘크리트 계면특성을 고려하는 것이 보다 합리적인 해석방법인 것으로 나타났다.

• 한국광학회지
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• 제9권6호
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• pp.408-412
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• 1998

곡선형 광도파로의 곡률반경이 작아짐에 따라 도파모드와 전파상수의 변화가 심화되므로 이종도파로 접합부에서의 모드 부정합이 손실을 유발하는 문제가 심각해졌다. 따라서, 곡률반경 변화에 따른 도파로의 모드 부정합을 극소화하기 위하여 이종 도파로간 lateral offset 이 제안되어 이의 계산이 여러 가지 방법으로 수행되어 왔는데, 본 논문에서는 유효 굴절률법(Effective index method)을 활용하고, Airy 함수로 주어지는 해석적 함수해의 분석을 통하여 곡률반경에 따른 전파모드의 특성변화와 lateral offset 거리의 변화를 분석하였다. 1/V=0.7인 특정조건을 경계로 모드분포의 특성이 바뀌며, 기존의 Gaussian 분석법에 의한 계산결과는 35%까지도 오차가 증대될 수 있음을 보였다. 새로이 오차보정상수(correction factor)η를 정의하여 기존 근사방식의 오차를 정량화하고, 간편히 도파로의 lateral offset을 설계 할 수 있도록 개선된 lateral offset 계산안을 제안하여 타당성을 보였다.

• 한국군사과학기술학회지
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• 제20권3호
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• pp.384-392
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• 2017

A linear explosively formed penetrator(LEFP) is a modification of the explosively formed penetrator(EFP). An EFP is axisymmetric and has a dish-shaped liner while LEFP has a rectangular-shaped liner with curved cross section. Upon detonating LEFP forms laterally wide projectile like blade, leaving a long penetration hole on the target. On the other hand, a long-rod tungsten heavy alloy(WHA) penetrator is one of the major threats against most of the ground armored vehicles. In this paper, the feasibility of using an LEFP in protecting against a long-rod WHA penetrator by colliding LEFP into the threat was investigated through a set of numerical simulations. In this study, a scale-down WHA penetrator with length to diameter ratio(L/D) of 10.7 and 7.0 mm diameter was used to represent a long-rod WHA penetrator. LS-DYNA and Multi-Material ALE technique were employed for the simulation. For estimation of the protection effect by LEFP, residual penetration depths into RHA by the threat were compared according to various impact locations against the threat.