• Journal of Pharmaceutical Investigation
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• 제14권2호
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• pp.62-69
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• 1984

Three-ply walled microcapsules containing furosemide and reserpine were prepared from multiple emulsion, and the the appearance of multiple emulsion, the particle size distribution and the drug contents of microcapsules were studied. The microcapsule consisted of alternating three layer of acacia/ethyl cellulose/acacia, and the surface of microcapsules was not porous but wrinkles and had relatively elaborate structure and the particle size range is $4{\mu}m$ to $64{\mu}m$.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2001년도 가을 학술발표회 논문집
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• pp.361-368
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• 2001

This paper deals with the buckling load of antisymmetric angle-ply and cross-ply laminated rectangular plates. Buckling analysis is preformed for a simply supported, shear deformable laminated plate subjected to uniaxial compression and biaxial compression combined with uniform lateral pression. The shear deformation theory is considered to figure out a more exact behavior of laminated plates exactly. The purposes of this study are to formulate anisotropic laminated plates with shear deformation and to investigate the buckling load according to the various variables of laminated plates by using the exact solutions for anisotropic laminated plates having simply supported boundary.

• Steel and Composite Structures
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• 제34권1호
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• pp.141-154
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• 2020

In the present paper, free vibration analysis of angle-ply laminated composite annular and circular plates is performed by numerical methods. First-order shear deformation plate theory is used for kinematic relations. The related governing equations of motion are discretized via differential quadrature and discrete singular convolution methods. Frequency values are obtained for different lamina scheme, thickness-to-radius ratio, and mode numbers. The advantages and accuracy of these two methods are also tested in detail.

• 항공우주시스템공학회지
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• 제1권4호
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• pp.28-36
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• 2007

This paper presents critical buckling loads of laminated composites under cylindrical bending. In-plane displacements are assumed to vary exponentially through plate thickness. The accuracy of this theory is examined for symmetric/antisymmetric cross-ply, angle-ply and unsymmetric laminates under cylindrical bending. Analytical solutions are provided to investigate the effect of transverse shear deformation on critical buckling loads of the laminated plates, and the results are compared with those obtained from the first-order shear deformation plate theory and the classical laminated plate theory.

• 한국군사과학기술학회지
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• 제2권2호
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• pp.271-278
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• 1999

An alternative panel flutter approach utilizing minimum angle is presented. The minimum angle is the lowest value among the angles between modes i and j at a certain pressure condition. This method utilizes eigenvectors rather than eigenvalues. Cross-ply composite plates are considered in this study. A remarkable result of this investigation is that the angle always dropped gradually to zero for all presented examples

• 타이어
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• 통권11호
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• pp.6-13
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• 1968

• 타이어
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• 통권11호
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• pp.17-18
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• 1968

• 타이어
• /
• 통권12호
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• pp.4-8
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• 1968

• 타이어
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• 통권2호
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• pp.14-15
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• 1967

• 타이어
• /
• 통권1호
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• pp.46-46
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• 1967