• 한국항해항만학회지
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• 제27권4호
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• pp.465-469
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• 2003

레이더 신호처리론 포함하여 무선통신 시스템의 성능향상을 위한 수신신호의 도래방향 추정기술 중, MUSIC과 ESPRIT와 같은 방법들은 수신신호 벡터로부터 얻어진 상관행렬의 고유치 분해를 통하여 도래방향을 정도 높게 추정할 수 있는 초고분해 알고리즘들로 잘 이용되어 왔다. 그러나, 이러한 방법들은 계산의 복잡성으로 인하여 실시간 처리에 장애가 되어 왔으며, 어레이 안테나의 물리적인 결함에 대한 보정을 요구한다. 이에 대한 해결방법으로서 신경망 모델을 이용한 도래방향 추정방법들이 연구되어 왔으나, 복수의 신호가 존재할 경우 신경망 모델에 대한 대규모 학습량을 요구하고, 실시간 처리가능성에 대한 명확한 해를 제공하지 못한다. 본 연구에서는 상호결합형 신경망 모델을 이용하여 도래방향을 추정하기 위한 방법을 제안하고, 컴퓨터 시뮬레이션을 통하여 실시간 처리가능성을 보여주었으며, 제안된 방법이 MUSIC 보다 더 좋은 추정치를 제공한다. 게다가, 제안된 방법은 대규모 학습을 요구하지 않는다. 즉, 도래방향을 추정하기 전에 상호결합계수를 신경망에 할당할 뿐이다.

• Structural Engineering and Mechanics
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• 제57권5호
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• pp.837-859
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• 2016

An efficient shear deformation theory is developed for wave propagation analysis of an infinite functionally graded plate in the presence of thermal environments. By dividing the transverse displacement into bending and shear parts, the number of unknowns and governing equations of the present theory is reduced, and hence, makes it simple to use. The thermal effects and temperature-dependent material properties are both taken into account. The temperature field is assumed to be a uniform distribution over the plate surface and varied in the thickness direction only. Material properties are assumed to be temperature-dependent, and graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents. The governing equations of the wave propagation in the functionally graded plate are derived by employing the Hamilton's principle and the physical neutral surface concept. There is no stretching.bending coupling effect in the neutral surface-based formulation, and consequently, the governing equations and boundary conditions of functionally graded plates based on neutral surface have the simple forms as those of isotropic plates. The analytic dispersion relation of the functionally graded plate is obtained by solving an eigenvalue problem. The effects of the volume fraction distributions and temperature on wave propagation of functionally graded plate are discussed in detail. It can be concluded that the present theory is not only accurate but also simple in predicting the wave propagation characteristics in the functionally graded plate. The results carried out can be used in the ultrasonic inspection techniques and structural health monitoring.

• Steel and Composite Structures
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• 제25권2호
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• pp.157-175
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• 2017

The novelty of this work is the use of a new displacement field that includes undetermined integral terms for analyzing thermal buckling response of functionally graded (FG) sandwich plates. The proposed kinematic uses only four variables, which is even less than the first shear deformation theory (FSDT) and the conventional higher shear deformation theories (HSDTs). The theory considers a trigonometric variation of transverse shear stress and verifies the traction free boundary conditions without employing the shear correction factors. Material properties of the sandwich plate faces are considered to be graded in the thickness direction according to a simple power-law variation in terms of the volume fractions of the constituents. The core layer is still homogeneous and made of an isotropic material. The thermal loads are assumed as uniform, linear and non-linear temperature rises within the thickness direction. An energy based variational principle is employed to derive the governing equations as an eigenvalue problem. The validation of the present work is checked by comparing the obtained results the available ones in the literature. The influences of aspect and thickness ratios, material index, loading type, and sandwich plate type on the critical buckling are all discussed.

• Steel and Composite Structures
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• 제31권5호
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• pp.503-516
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• 2019

This work presents a dynamic investigation of functionally graded (FG) plates resting on elastic foundation using a simple quasi-3D higher shear deformation theory (quasi-3D HSDT) in which the stretching effect is considered. The culmination of this theory is that in addition to taking into account the effect of thickness extension (${\varepsilon}_z{\neq}0$), the kinematic is defined with only 4 unknowns, which is even lower than the first order shear deformation theory (FSDT). The elastic foundation is included in the formulation using the Pasternak mathematical model. The governing equations are deduced through the Hamilton's principle. These equations are then solved via closed-type solutions of the Navier type. The fundamental frequencies are predicted by solving the eigenvalue problem. The degree of accuracy of present solutions can be shown by comparing it to the 3D solution and other closed-form solutions available in the literature.

• Geomechanics and Engineering
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• 제18권1호
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• pp.85-96
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• 2019

A free vibration analysis and wave propagation of triclinic and orthotropic plate has been presented in this work using an efficient quasi 3D shear deformation theory. The novelty of this paper is to introducing this theory to minimize the number of unknowns which is three; instead four in other researches, to studying bulk waves in anisotropic plates, other than it can model plates with great thickness ratio, also. Another advantage of this theory is to permits us to show the effect of both bending and shear components and this is carried out by dividing the transverse displacement into the bending and shear parts. Hamilton's equations are a very potent formulation of the equations of analytic mechanics; it is used for the development of wave propagation equations in the anisotropic plates. The analytical dispersion relationship of this type of plate is obtained by solving an eigenvalue problem. The accuracy of the present model is verified by confronting our results with those available in open literature for anisotropic plates. Moreover Numerical examples are given to show the effects of wave number and thickness on free vibration and wave propagation in anisotropic plates.

• 항공우주시스템공학회지
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• 제16권3호
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• pp.63-72
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• 2022

본 논문에서는 전개형 메쉬 안테나의 동적 강성 설계 및 다물체 동역학을 이용한 요구되는 구동력 및 전개 특성을 분석하고자 한다. 프레임(frame) 요소를 이용하여 전개 구조물을 모델링한다. 다각(polygon) 형상 전개 구조물의 전개/수납된 형상에 따른 고유치 문제를 분석하였다. Kane's 방정식을 이용하여 전개 구조물의 다물체 동역학 방정식을 유도하고 PUTD (pseudo upper triangular decomposition) 방법을 적용하여 구속조건 문제를 해결하였다. 고유진동 해석 및 다물체 동역학 시뮬레이션을 통해 설계된 전개형 구조의 구조 동특성 및 실현성을 살펴보고자 한다.

• Advances in aircraft and spacecraft science
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• 제8권4호
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• pp.345-372
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• 2021

The analysis of nonlinear vibrations, buckling, post-buckling, flutter boundary determination and post-flutter behavior of a homogeneous curved plate assuming cylindrical bending is conducted in this article. Other assumptions include simply-supported boundary conditions, supersonic aerodynamic flow at the top of the plate, constant pressure conditions below the plate, non-viscous flow model (using first- and third-order piston theory), nonlinear structural model with large deformations, and application of mechanical and thermal loads on the curved plate. The analysis is performed with constant environmental indicators (flow density, heat, Reynolds number and Mach number). The material properties (i.e., coefficient of thermal expansion and modulus of elasticity) are temperature-dependent. The equations are derived using the principle of virtual displacement. Furthermore, based on the definitions of virtual work, the potential and kinetic energy of the final relations in the integral form, and the governing nonlinear differential equations are obtained after fractional integration. This problem is solved using two approaches. The frequency analysis and flutter are studied in the first approach by transferring the handle of ordinary differential equations to the state space, calculating the system Jacobin matrix and analyzing the eigenvalue to determine the instability conditions. The second approach discusses the nonlinear frequency analysis and nonlinear flutter using the semi-analytical solution of governing differential equations based on the weighted residual method. The partial differential equations are converted to ordinary differential equations, after which they are solved based on the Runge-Kutta fourth- and fifth-order methods. The comparison between the results of frequency and flutter analysis of curved plate is linearly and nonlinearly performed for the first time. The results show that the plate curvature has a profound impact on the instability boundary of the plate under supersonic aerodynamic loading. The flutter boundary decreases with growing thermal load and increases with growing curvature.

• Coupled systems mechanics
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• 제12권1호
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• pp.41-68
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• 2023

The present work is concerned with the study of the influence of inhomogeneous initial stresses in a hollow cylinder containing a compressible inviscid fluid on the propagation of axisymmetric longitudinal waves propagating in this cylinder. The study is carried out using the so-called three-dimensional linearized theory of elastic waves in bodies with initial stresses to describe the motion of the cylinder and using the linearized Euler equations to describe the flow of the compressible inviscid fluid. It is assumed that the inhomogeneous initial stresses in the cylinder are caused by the internal pressure of the fluid. To solve the corresponding eigenvalue problem, the discrete-analytic solution method is applied and the corresponding dispersion equation is obtained, which is solved numerically, after which the corresponding dispersion curves are constructed and analyzed. To obtain these dispersion curves, parameters characterizing the magnitude of the internal pressure, the ratio of the sound velocities in the cylinder material and in the fluid, and the ratio of the material densities of the fluid and the cylinder are introduced. Based on these parameters, the influence of the inhomogeneous initial stresses in the cylinder on the dispersion of the above-mentioned waves in the considered hydro-elastic system is investigated. Moreover, based on these results, appropriate conclusions about this influence are drawn. In particular, it is found that the character of the influence depends on the wavelength. Accordingly, the inhomogeneous initial stresses before (after) a certain value of the wavelength lead to a decrease (increase) of the wave propagation velocity in the zeroth and first modes.

• Steel and Composite Structures
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• 제45권2호
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• pp.175-191
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• 2022

A review of previous studies shows that although there is a considerable difference between buckling loads of structures under follower and non-follower lateral loads, only the buckling load of FGM elliptical cylindrical shell under non-follower lateral load was investigated in the literature. This study is the first to obtain the buckling load of elliptical FGM cylindrical shells under follower lateral load and also make a comparison between buckling loads of elliptical FGM cylindrical shells under follower and non-follower lateral loads. Moreover, this research is the first one to derive the load potential function of elliptical cylindrical shell. In this regard, the FGM cylindrical elliptical shell was modeled using the semi-analytical finite strip method and based on the First Shear Deformation Theory (FSDT). The shell is discretized by strip elements aligned in the longitudinal direction. The Lagrangian and harmonic shape functions were considered in the circumference and longitudinal directions, respectively. The buckling pressure of the shell under follower and non-follower lateral loads was obtained from eigenvalue problem. The results obtained from the model were compared with those presented in the literature to evaluate the validity of the model. A comparison index was defined to compare the buckling loads of the shell under follower and non-follower lateral load. A parametric study was carried out to investigate the effects of material properties and shell geometry characteristics on the comparison index. For the elliptical cylindrical shells with length-to-radius ratio greater than 16 and major-to-minor axis ratio greater than 0.6, the comparison index reaches to more than 20 percent which is significant. Moreover, the maximum difference is about 30 percent in some cases. The results obtained from the parametric study indicate that the buckling load of long elliptical cylindrical shell under non-follower load is not reliable.

• 한국전산구조공학회논문집
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• 제16권2호
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• pp.197-206
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• 2003

임의의 경계조건과 변두께를 갖는 축대칭 반구형 쉘과 반구형체의 진동수와 모우드형상을 결정하는 3차원적 해석법이 소개되었다. 수학적으로 2차원적인 전통적인 쉘이론과는 달리 본 연구의 해석법은 3차원 동적 탄성방정식을 사용하였다 자오선방향 (Φ), 법선방향(z), 원주방향(θ)으로의 변위성분인 μ/sub Φ/, μ/sub z/, μ/sub θ/는 시간에 대해서는 정현적으로, θ에 대해서는 주기적으로, 와 z 방향에 대해서는 대수다항식으로 표현될 수 있다. 축대칭 반구형 쉘의 변형률 에너지와 운동 에너지를 정식화하고, 리츠법으로 고유치문제를 계산하였다. 진동수의 최소화과정을 통해 엄밀해의 상위 경계치 진동수를 구하였으며, 이 때, 다항식의 차수를 증가시키면 진동수는 엄밀해에 수렴하게 된다. 자오선방향으로 선형적으로 꿩 두께가 변하는 반구형 쉘과 반구형체치 3차원적 진동수를 최초로 계산하였으며, 축방향으로 난 조그만 원추형 구멍이 진동수에 미치는 영향도 분석하였다. 상두께와 자유경계조건을 갖는 두꺼운 축대칭 반구형 쉘에 대한 3차원적 리츠해와 3차원적 유한요소법에 의한 진동수를 서로 비교하였다.