• Title/Summary/Keyword: 3D effect

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Effect of [6]-Gingerol, a Pungent Ingredient of Ginger, on Osteoblast Response to Extracellular Reducing Sugar

  • Kim, Young-Ho;Nguyen, Huu Thng;Ding, Yan;Park, Sang-Heock;Choi, Eun-Mi
    • Food Science and Biotechnology
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    • v.16 no.5
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    • pp.807-811
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    • 2007
  • Diabetes is marked by high glucose levels and is associated with decreased bone mass and increased fracture rates. To determine if [6]-gingerol could influence osteoblast dysfunction induced by 2-deoxy-D-ribose (dRib), osteoblastic MC3T3-E1 cells was treated with dRib and [6]-gingerol and markers of osteoblast function and oxidized protein were examined. [6]-Gingerol ($10^{-7}\;M$) significantly increased the growth of MC3T3-E1 cells in the presence of 30 mM dRib (p<0.05). [6]-Gingerol ($10^{-7}\;M$) caused a significant elevation of alkaline phosphatase (ALP) activity, collagen content, and osteocalcin secretion in the cells. We then examined the effect of [6]-gingerol on the production of osteoprotegerin and protein carbonyl in osteoblasts. Treatment with [6]-gingerol ($10^{-9}$ and $10^{-7}\;M$) increased osteoprotegerin secretion in osteoblastic cells. Moreover, [6]-gingerol ($10^{-9}$ and $10^{-7}\;M$) decreased protein carbonyl contents of osteoblastic MC3T3-E1 cells in the presence of 30 mM dRib. Taken together, these results demonstrate that [6]-gingerol inhibits dRib-induced damage and may be useful in the treatment of diabetes related bone diseases.

Boundary Layer Separation Control with Fairing at the Junction of 3D Wings Under Ground Effect (페어링을 이용한 지면효과를 받는 3차원 날개 접합부의 경계층 박리 제어)

  • Cho Ji. H.;Moon Young. J.
    • 한국전산유체공학회:학술대회논문집
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    • 2005.04a
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    • pp.57-64
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    • 2005
  • Aerodynamic characteristics of three-dimensional wings in ground effect for Aero-levitation Electric Vehicle(AEV) are numerically investigated for various fairing shapes at the junctions of 3D Wings. Numerical results show that a sizeable three-dimensional comer flow separation occurs with formation of an arch vortex at the junction of main and vertical wings, and also that this is predicted the main cause of the high lift-to-drag(L/D) reduction rate of the main wing. To avoid the comer flow separation, the main idea of this study is to reduce the cross section gradient of the comer flow tube near the trailing edge for various fairing shapes. Improvements on L/D ratios of the wings are pursued by breaking the coherence of superimposed adverse pressure gradients at the wing junction when the cross section gradient is changed slowly at the trailing edge.

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Effect of Three-dimensional Warping on Stiffness Constants of Closed Section Composite Beams

  • Dhadwal, Manoj Kumar;Jung, Sung Nam
    • International Journal of Aeronautical and Space Sciences
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    • v.18 no.3
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    • pp.467-473
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    • 2017
  • This paper focuses on the investigation of three-dimensional (3D) warping effect on the stiffness constants of composite beams with closed section profiles. A finite element (FE) cross-sectional analysis is developed based on the Reissner's multifield variational principle. The 3D in-plane and out-of-plane warping displacements, and sectional stresses are approximated as linear functions of generalized sectional stress resultants at the global level and as FE shape functions at the local sectional level. The classical elastic couplings are taken into account which include transverse shear and Poisson deformation effects. A generalized Timoshenko level $6{\times}6$ stiffness matrix is computed for closed section composite beams with and without warping. The effect of neglecting the 3D warping on stiffness constants is shown to be significant indicating large errors as high as 93.3%.

Effect of Multi-directional Random Waves on Characteristics of 3-D Wave Field around Permeable Submerged Breakwaters (다방향 불규칙파가 투과성 잠제 주변의 3차원 파동장에 미치는 영향)

  • Hur, Dong-Soo;Lee, Woo-Dong
    • Journal of Ocean Engineering and Technology
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    • v.26 no.2
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    • pp.68-78
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    • 2012
  • This study proposes an improved 3-D model that includes a new non-reflected wave generation system for oblique incident and multi-directional random waves, which enables us to estimate the effect of the various wave-types on 3-D wave fields in a coastal area with permeable submerged breakwaters. Then, using the numerical results,the three-dimensional wave field characteristics around permeable submerged breakwaters are examined in cases of oblique incident and multi-directional random waves. Especially, the wave height, mean surface elevation and mean flow around the submerged breakwaters are discussed in relation to the variation of incident wave condition.

Effects of Titanium, Hafnium and Zircornium Alloying Elements on Microstructures and $D0_3{\leftrightarrow}B2$ Transition Temperature of Fe-30Al-5Cr Alloys (Fe-30Al-5Cr 합금의 미세조직 및 $D0_3{\leftrightarrow}B2$ 천이온도에 미치는 Ti, Hf 및 Zr의 첨가효과)

  • Kim, Sung-Su;Joo, Sung-Min;Oh, Seon-Hun;Kim, Kwan-Hyu;Choi, Dap-Chun
    • Journal of Korea Foundry Society
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    • v.21 no.1
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    • pp.15-23
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    • 2001
  • The changes in the microstructures and $D0_3{\leftrightarrow}B2$ transition temperature were investigated for Fe-30at.%AI-5at.%Cr alloy with the ordered $D0_3$, structure when Ti, Hf and Zr were added respectively. The addition of Cr has no effect on the microstructure. However, as the amount of Ti addition increased, the grain size became smaller. Addition of Ti+Hf, Ti+Zr and Ti+Hf+Zr also showed the similar effect. When 20at.% of Ti was added, the second phase precipitates on the substrate. The addition of Cr, Hf and Zr alone has no effect on $D0_3{\leftrightarrow}B2$ transition temperature. However, as the amount of Ti addition increased by 5, 10, 15 and 20at.%, the transition temperatures showed 929, 930, 960 and $930^{\circ}C$ respectively.

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Improving VRML/X3D Fog Effect Using Distance Coefficient (Distance coefficient를 ol용한 VRML/X3D 안개효과 개선)

  • 박승규;진성아;김성동
    • Proceedings of the Korea Multimedia Society Conference
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    • 2003.11b
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    • pp.593-596
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    • 2003
  • 웹상의 3차원 세계를 구현할 수 있는 국제표준 언어인 VRML/X3D를 이용한 Web3D콘텐츠의 요구가 증대되고 있다. 본 논문은 VRMI/X3D에서 지원하는 안개(Fog)효과의 한계를 고찰하고 효과적인 안개효과를 개선할 수 있는 방법을 제안한다 거리계수를 파라미터로 사용함으로서 지역적인 안개의 표현과 다양한 안계밀도를 생성하는 방법을 실험하였다.

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A study on consumer attitudes and purchase intentions for 3D printed products in the fashion industry (패션산업에서 3D 프린트 제품에 대한 소비자 태도 및 구매의도연구)

  • Kim, Jisoo;Shin, Sangmoo
    • The Research Journal of the Costume Culture
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    • v.26 no.6
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    • pp.919-933
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    • 2018
  • Recently, the textile and fashion industry has adopted 3D printing technology, through which filaments are accumulated continuously in the form of sections to produce digitalized three-dimensional fashion products. Little research has been done regarding the consumer perspectives on 3D printed fashion product. Therefore, the purpose of this study was to investigate the effects of consumer innovativeness, uniqueness, and perception factors on consumer attitudes and purchasing intentions for 3D printed fashion products. A questionnaire was given to consumers living in Seoul and Kyunggi, South Korea. The data obtained from the 159 completed questionnaires was analyzed by regression analysis, factor analysis, and Cronbach's alpha using SPSS 24.0. The results were as follows: First, consumer innovativeness and uniqueness, in descending order, positively affect the perceived social image. Consumer innovativeness positively affects perceived aesthetics and consumer uniqueness positively affects perceived novelty. Second, social image has a positive effect on consumer attitudes to 3D printed fashion products. Third, consumer attitude positively affects purchasing intentions towards 3D printed fashion products. Fourth, consumer innovativeness and uniqueness, in descending order, have a positive effect on consumer attitudes and purchasing intentions for 3D printed fashion products. Fifth, social image and novelty, in descending order, positively affect purchase intentions for 3D printed fashion products. Therefore fashion firms should develop their marketing strategy to focus on innovative, unique consumers as a main target and aim to enhance buyers' social image by using 3D printed fashion products.

Effect of Bulk Shape on Mechanical Properties of Ti-6Al-4V Alloy Manufactured by Laser Powder Bed Fusion (Laser Powder Bed Fusion 공정으로 제조된 Ti-6Al-4V 합금의 형상 차이에 따른 기계적 특성 변화)

  • Haeum Park;Yeon Woo Kim;Seungyeon Lee;Kyung Tae Kim;Ji-Hun Yu;Jung Gi Kim;Jeong Min Park
    • Journal of Powder Materials
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    • v.30 no.2
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    • pp.140-145
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    • 2023
  • Although the Ti-6Al-4V alloy has been used in the aircraft industry owing to its excellent mechanical properties and low density, the low formability of the alloy hinders broadening its applications. Recently, laser-powder bed fusion (L-PBF) has become a novel process for overcoming the limitations of the alloy (i.e., low formability), owing to the high degree of design freedom for the geometry of products having outstanding performance used in high-tech applications. In this study, to investigate the effect of bulk shape on the microstructure and mechanical properties of L-PBFed Ti-6Al-4V alloys, two types of samples are fabricated using L-PBF: thick and thin samples. The thick sample exhibits lower strength and higher ductility than the thin sample owing to the larger grain size and lower residual dislocation density of the thick sample because of the heat input during the L-PBF process.

Axial Turbine Aerodynamic Design of Small Heavy-Duty Gas Turbines (발전용 소형가스터빈의 축류터빈 공력설계)

  • Kim, Joung Seok;Lee, Wu Sang;Ryu, Je Wook
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.37 no.4
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    • pp.415-421
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    • 2013
  • This study describes the aerodynamic design procedure for the axial turbines of a small heavy-duty gas turbine engine being developed by Doosan Heavy Industries. The design procedure mainly consists of three parts: namely, flowpath design, airfoil design, and 3D performance calculation. To design the optimized flowpath, through-flow calculations as well as the loss estimation are widely used to evaluate the effect of geometric variables, for example, shape of meridional plane, mean radius, blades axial gap, and hade angle. During the airfoil design procedure, the optimum number of blades is calculated by empirical correlations based on the in/outlet flow angles, and then 2D airfoil planar sections are designed carefully, followed by 2D B2B NS calculations. The designed planar sections are stacked along the spanwise direction, leading to a 3D surfaced airfoil shape. To consider the 3D effect on turbine performance, 3D multistage Euler calculation, single row, and multistage NS calculations are performed.