• Structural Engineering and Mechanics
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• 제54권4호
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• pp.693-710
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• 2015

This paper presents a nonlocal shear deformation beam theory for bending, buckling, and vibration of functionally graded (FG) nanobeams using the nonlocal differential constitutive relations of Eringen. The developed theory account for higher-order variation of transverse shear strain through the depth of the nanobeam, and satisfy the stress-free boundary conditions on the top and bottom surfaces of the nanobeam. A shear correction factor, therefore, is not required. In addition, this nonlocal nanobeam model incorporates the length scale parameter which can capture the small scale effect and it has strong similarities with Euler-Bernoulli beam model in some aspects such as equations of motion, boundary conditions, and stress resultant expressions. The material properties of the FG nanobeam are assumed to vary in the thickness direction. The equations of motion are derived from Hamilton's principle. Analytical solutions are presented for a simply supported FG nanobeam, and the obtained results compare well with those predicted by the nonlocal Timoshenko beam theory.

• 대한기계학회논문집B
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• 제22권2호
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• pp.240-252
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• 1998

The purpose of this study is to develop a method for predicting the aerodynamic performance of the low speed airfoils in the 2-dimensional, steady and viscous flow. For this study, the airfoil geometry is specified by adopting the longest chord line system and by considering local surface curvature. In case of the inviscid incompressible flow, the analysis is accomplished by the linearly varying strength vortex panel method and the Karman-Tsien correction law is applied for the inviscid compressible flow analysis. The Goradia integral method is adopted for the boundary layer analysis of the laminar and turbulent flows. Viscous and inviscid solutions are converged by the Lockheed iterative calculating method using the equivalent airfoil geometry. The analysis of the separated flow is performed using the Dvorak and Maskew's method as the basic method. The wake effect is also considered by expressing its geometry using the formula of Summey and Smith when no separation occurs. The computational efficiency is verified by comparing the computational results with experimental data and by the shorter execution time.

• Steel and Composite Structures
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• 제33권1호
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• pp.81-92
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• 2019

The present paper addresses a refined plate theoryin order to describe the response of anti-symmetric cross-ply laminated plates subjected to a uniformlydistributed nonlinear thermo-mechanical loading. In the present theory, the undetermined integral terms are used and the variables number is reduced to four instead of five or more in other higher-order theories. The boundary conditions on the top and the bottom surfaces of the plate are satisfied; hence the use of the transverse shear correction factors isavoided. The principle of virtual work is used to obtain governing equations and boundary conditions. Navier solution for simply supported plates is used to derive analytical solutions. For the validation of the present theory, numerical results for displacements and stressesare compared with those of classical, first-order, higher-order and trigonometricshear theories reported in the literature.

• Nuclear Engineering and Technology
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• 제51권5호
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• pp.1209-1217
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• 2019

Due to the limitation of the computers, the conventional homogenization method is based on many assumptions and approximations, and some tough problems such as energy spectrum and boundary condition are faced. To deal with those problems, the Monte Carlo global homogenization is adopted. The Reactor Monte Carlo code RMC is used to study the global homogenization method, and the one-step global homogenization method is proposed. The superimposed mesh geometry is also used to divide the physical models, leading to better geometric flexibility. A set of multigroup homogenization cross sections is online generated for each mesh under the real neutron energy spectrum and boundary condition, the cross sections are adjusted by the superhomogenization method, and no leakage correction is required. During the process of superhomogenization, the author-developed reactor core program NLSP3 is used for global calculation, so the global flux distribution and equivalent homogenization cross sections could be solved simultaneously. Meanwhile, the calculated homogenization cross section could accurately reconstruct the non-homogenization flux distribution and could also be used for fine calculation. This one-step global homogenization method was tested by a PWR assembly and a small reactor model, and the results show the validity.

• Advances in aircraft and spacecraft science
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• 제6권5호
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• pp.409-426
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• 2019

The aim of the present work is to study the nonlinear behavior of the laminated composite plates under transverse sinusoidal loading using a new inverse trigonometric shear deformation theory, where geometric nonlinearity in the Von-Karman sense is taken into account. In the present theory, in-plane displacements use an inverse trigonometric shape function to account the effect of transverse shear deformation. The theory satisfies the traction free boundary conditions and violates the need of shear correction factor. The governing equations of equilibrium and boundary conditions associated with present theory are obtained by using the principle of minimum potential energy. These governing equations are solved by eight nodded serendipity element having five degree of freedom per node. A square laminated composite plate is considered for the geometrically linear and nonlinear formulation. The numerical results are obtained for central deflections, in-plane stresses and transverse shear stresses. Finite element Codes are developed using MATLAB. The present results are compared with previously published results. It is concluded that the geometrically linear and nonlinear response of laminated composite plates predicted by using the present inverse trigonometric shape function is in excellent agreement with previously published results.

• Structural Engineering and Mechanics
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• 제77권1호
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• pp.103-114
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• 2021

Ultra high strength concrete (UHSC) originally proposed by Richards and Cheyrezy (1995) composed of cement, silica fume, quartz sand, quartz powder, steel fibers, superplasticizer etc. Later, other ingredients such as fly ash, GGBS, metakaoline, copper slag, fine aggregate of different sizes have been added to original UHSC. In the present investigation, the combined effect of coarse aggregate (6mm - 10mm) and steel fibers (0.50%, 1.0% and 1.5%) has been studied on UHSC mixes to evaluate mechanical and fracture properties. Compressive strength, split tensile strength and modulus of elasticity were determined for the three UHSC mixes. Size dependent fracture energy was evaluated by using RILEM work of fracture and size independent fracture energy was evaluated by using (i) RILEM work of fracture with tail correction to load - deflection plot (ii) boundary effect method. The constitutive relationship between the residual stress carrying capacity (σ) and the corresponding crack opening (w) has been constructed in an inverse manner based on the concept of a non-linear hinge from the load-crack mouth opening plots of notched three-point bend beams. It was found that (i) the size independent fracture energy obtained by using above two approaches yielded similar value and (ii) tensile stress increases with the increase of % of fibers. These two fracture properties will be very much useful for the analysis of cracked concrete structural components.

• 대한원격탐사학회지
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• 제34권3호
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• pp.451-463
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• 2018

본 연구는 서울지역에서 2015년 1월부터 12월까지 정지궤도 천리안 위성(Communication Ocean and Meteorological Satellite, COMS) 해양 탑재체(Geostationary Ocean Color Imager, GOCI)의 에어로졸광학두께(Aerosol Optical Depth, AOD)로부터 지상 초미세먼지(Particulate Matter; $PM_{2.5}$) 농도를 추정하기 위한 계절별 경험/통계모델을 개발했다. 행성경계층고도(Planetary Boundary Layer Height, PBLH) 그리고 에어로졸 수직 비율(Vertical Ratio of Aerosol, VRA)을 사용한 두 가지 수직보정방법과 흡습성장계수(Hygroscopic growth factor, f(RH))로부터의 습도보정방법이 각각의 경험적 모델에 적용된 결과 AOD에 대한 수직 보정과 $PM_{2.5}$에 대한 지표 습도보정이 모델 성능 향상에 중요한 역할을 했다. AOD-$PM_{2.5}$ 사이에 관련이 있다고 알려진 기상인자들(온도, 풍속, 시정)을 추가적으로 사용하여 다중 선형 회귀모델을 구성한 결과 경험모델에 비해 $R^2$값이 최대 0.25 증가했다. 본 연구에선 AOD-$PM_{2.5}$ 모델의 계절별, 월별, 시간별 특성을 분석하고 계절별로 구분하여 모델을 구성한 결과 고농도 사례에서 과소평가 되던 경향이 개선됨을 알 수 있고 관측된 $PM_{2.5}$와 추정된 $PM_{2.5}$의 월 및 시간변동성은 서로 경향성이 일치했다. 따라서 정지궤도 위성 AOD를 이용하여 지상 $PM_{2.5}$ 농도를 추정한 본 연구의 결과는 향후 발사 예정인 GK-2A와 GK-2B에 적용 가능할 것으로 기대된다.

• 대한전자공학회논문지SP
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• 제49권2호
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• pp.35-44
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• 2012

대부분의 최근 적외선 센서는 focal-plane array (FPA) 구조로 되어있다. 이러한 구조의 센서는 공간적 불균일 응답성을 갖는 것으로 알려져 있고, 이로 인해 고정패턴잡음을 발생시킴으로써 영상열화를 가져온다. 따라서 적외선 영상의 고정패턴잡음을 제거하기 위해서는 픽셀 불균일 보정을 해야 한다. 픽셀 불균일 보정기법은 참조물체기반 접근법과 영상기반 접근법으로 나눌 수 있다. 참조물체기반 접근법에서는 흑체와 같은 균일한 온도를 갖는 물체를 이용해서 고정패턴잡음을 분리시킬 수 있는 방법이다. 하지만 센서의 응답성은 시간이 지나면서 변할 수 있기 때문에, 최근에는 비디오 영상을 이용하는 영상기반 접근법이 많이 연구되고 있다. 영상기반 접근법들 중에서 칼만 필터를 기반으로 하는 최신 알고리듬은 영상 간에 움직임 보상 시에 한 방향 워핑을 이용하고 센서의 offset 불균일성만을 보상해준다. 하지만 한 방향 워핑을 이용한 시스템 모델은 영상의 경계 부근에서 고정패턴잡음을 효과적으로 제거하지 못한다. 게다가, offset만 보정하는 접근법은 gain의 불균일성의 영향을 많이 받는 영상에서는 성능이 악화될 수 있다. 그러므로 본 논문에서는 양방향 워핑을 이용하여 시스템 모델링을 하고, gain과 offset의 결합 보정을 수행하는 알고리듬을 제안한다. 모사 영상과 실제 영상에 대한 실험 결과들은 제안하는 알고리듬이 기존 알고리듬들보다 더 효과적으로 고정패턴잡음을 제거하는 것을 확인할 수 있다.

• Steel and Composite Structures
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• 제36권3호
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• pp.355-367
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• 2020

The current work, present dynamic analysis of the FG-sandwich plate seated on elastic foundation with various kinds of support using refined shear deformation theory. The present analytical model is simplified which the unknowns number are reduced. The zero-shear stresses at the free surfaces of the FG-sandwich plate are ensured without introducing any correction factors. The four equations of motion are determined via Hamilton's principle and solved by Galerkin's approach for FG-sandwich plate with three kinds of the support. The proposed analytical model is verified by comparing the results with those obtained by other theories existing in the literature. The parametric studies are presented to detect the various parameters influencing the fundamental frequencies of the symmetric and non-symmetric FG-sandwich plate with various boundary conditions.

• 한국항공우주학회지
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• 제40권2호
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• pp.171-177
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• 2012

본 논문에서는 항공기 탑재용 GNSS 수신기 고장검출 알고리즘과 운용범위를 제안하였다. 고장난 항공기 수신기는 항공기에서 계산한 보정정보를 주변 항공기간 상호 교환 후에, 보정정보 일치 여부를 통해 검출한다. 이를 위해, 항공기 수신기 고장검출 알고리즘에 사용되는 검정통계량으로 보정정보 잔차값을 사용하였으며, 운용범위는 지상 기준국을 중심으로 거리에 따른 DGPS 위치오차 증가량을 이용하여 설정하였다. 정확한 고장검출을 위해 운용범위 안의 항공기들만을 사용하여 항공기 탑재용 GNSS 수신기 고장검출을 시도하는 방안을 제안하였다.