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空间的尺度与比例 被引量:1
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作者 骆萌 《齐齐哈尔师范高等专科学校学报》 2005年第2期153-154,共2页
和谐的比例与尺度是建筑形态美的必要条件。建筑设计实际上是空间尺度、比例,布局的设计与空间渲染问题,了解人与空间、空间与空间的相互关系对与合理设计空间是非常必要的,否则设计出的空间会给人们的生活带来影响和不便。在建筑空间中... 和谐的比例与尺度是建筑形态美的必要条件。建筑设计实际上是空间尺度、比例,布局的设计与空间渲染问题,了解人与空间、空间与空间的相互关系对与合理设计空间是非常必要的,否则设计出的空间会给人们的生活带来影响和不便。在建筑空间中,应该遵循空间的比例与尺度的控制,空间的界面的处理。 展开更多
关键词 比例与尺度的协调 空间尺度 空间序列 比例度量
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Effect of Different Ratios of DL-type Starter Culture: Mould Geotrichum candidum on the Viscosity and Sensory Properties of Fermented Milk
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《Journal of Food Science and Engineering》 2011年第5期395-399,共5页
A great variety of dairy products with different flavour, texture and health-promoting properties can be obtained from milk using different technologies and starter cultures. Fermented milks are consumed in many parts... A great variety of dairy products with different flavour, texture and health-promoting properties can be obtained from milk using different technologies and starter cultures. Fermented milks are consumed in many parts of the world and are relished for their acidic taste and health benefits. The aim of this study was to compare effects of different ratios of DL-type starter culture: mould Geotrichum candidum grown in milk on its viscosity and sensory properties on the 5th, 10th and 15th day of storage at 4 ~C~ in order to determine the best ratio to prepare fermented milk on basis of Iranian acceptance. We have examined the production of fermented milk by 80: 20, 70: 30, and 60:40 ratios of DL-type starter culture: mould Geotrichum candidum grown in milk. The results obtained from viscosity measurement and sensory evaluation showed no significant difference between these treatments used in the study and were not satisfactory; their viscosity was not accepted and scores attributed to odour and flavor of fermented milks by panelists were low. 展开更多
关键词 Fermented milk Geotrichum candidum viili DL-type starter culture sensory properties viscosity.
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Parametric study on collapse margin ratio of structure
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作者 欧晓英 何政 欧进萍 《Journal of Central South University》 SCIE EI CAS 2014年第6期2477-2486,共10页
The determination of collapse margin ratio(CMR)of structure is influenced by many uncertain factors.Some factors that can affect the calculation of CMR,e.g.,the elongation of the structural fundamental period prior to... The determination of collapse margin ratio(CMR)of structure is influenced by many uncertain factors.Some factors that can affect the calculation of CMR,e.g.,the elongation of the structural fundamental period prior to collapse,the determination of earthquake intensity measure,the seismic hazard probability,and the difference of the spectral shapes between the median spectrum of the ground motions and the design spectrum,were discussed.Considering the elongation of the structural fundamental period,the intensity measure Sa(T1)should be replaced with *aS in the calculation of CMR for short-period and medium-period structures.The reasonable intensity measure should be determined by the correlation analysis between the earthquake intensity measure and the damage index of the structure.Otherwise,CMR should be adjusted according to the seismic hazard probability and the difference in the spectral shapes.For important long-period structures,CMR should be determined by the special site spectrum.The results indicate that both Sa(T1)and spectrum intensity(SI)could be used as intensity measures in the calculation of CMR for medium-period structures,but SI would be a better choice for long-period structures.Moreover,an adjusted CMR that reflects the actual seismic collapse safety of structures is provided. 展开更多
关键词 collapse margin ratio strong ground motion intensity measurement probability of exceedance Housner's spectrum intensity spectrum acceleration
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Symmetry Analysis of Barotropic Potential Vorticity Equation
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作者 Alexander Bihlo RomanO.Popovych 《Communications in Theoretical Physics》 SCIE CAS CSCD 2009年第10期697-700,共4页
Recently F. Huang [Commun. Theor. Phys. 42 (2004) 903] and X. Tang and P.K. Shukla [Commun. Theor. Phys. 49 (2008) 229] investigated symmetry properties of the barotropic potential vorticity equation without forci... Recently F. Huang [Commun. Theor. Phys. 42 (2004) 903] and X. Tang and P.K. Shukla [Commun. Theor. Phys. 49 (2008) 229] investigated symmetry properties of the barotropic potential vorticity equation without forcing and dissipation on the beta-plane. This equation is governed by two dimensionless parameters, F and β, representing the ratio of the characteristic length scale to the Rossby radius of deformation and the variation of earth' angular rotation, respectively. In the present paper it is shown that in the case F ≠ 0 there exists a well-defined point transformation to set β = 0. The classification of one- and two-dimensional Lie subalgebras of the Lie symmetry algebra of the potential vorticity equation is given for the parameter combination F ≠ 0 and β = 0. Based upon this classification, distinct classes of group-invariant solutions are obtained and extended to the case β ≠0. 展开更多
关键词 potential vorticity equation Lie symmetries classification of subalgebras exact solutions
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Aeroelastic optimization on composite skins of large aircraft wings 被引量:11
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作者 LIANG Lu WAN ZhiQiang YANG Chao 《Science China(Technological Sciences)》 SCIE EI CAS 2012年第4期1078-1085,共8页
This paper presents studies of aeroelastic optimization on composite skins of large aircraft wings subject to aeroelastic constraints and strength/strain constraints. The design variable for optimization was the ply t... This paper presents studies of aeroelastic optimization on composite skins of large aircraft wings subject to aeroelastic constraints and strength/strain constraints. The design variable for optimization was the ply thickness of the wing skin panels, and the structural weight was the objective function to be minimised. The impacts of three strength/strain constraints and the ply proportion of the wing skin panels on the optimization results are discussed. The results indicate that the optimal composite wings that satisfy different constraints have remarkable weight advantages over metal wing. High levels of stiffness can be achieved while satisfying the constraints regarding allowable design strains and failure criteria. The optimization results with variable-proportions indicate that wing skins with higher proportions of 0° plies from the root to the middle segment and ±45° plies outboard have a more efficient and reasonable stiffness distribution. 展开更多
关键词 aeroelastic optimization large aircraft composite wing strength constraints ply proportion
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Effects of the ZnO buffer layer and Al proportion on AZO film properties 被引量:5
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作者 隋成华 刘彬 +2 位作者 徐天宁 鄢波 魏高尧 《Optoelectronics Letters》 EI 2012年第3期205-208,共4页
To evaluate the influence of the ZnO buffer layer and A1 proportion on the properties of ZnO: A1 (AZO)/ZnO bi-layer films, a series of AZO/ZnO films are deposited on the quartz substrates by electron beam evaporati... To evaluate the influence of the ZnO buffer layer and A1 proportion on the properties of ZnO: A1 (AZO)/ZnO bi-layer films, a series of AZO/ZnO films are deposited on the quartz substrates by electron beam evaporation. The X-ray diffraction measurement shows that the crystal quality of the films is improved with the increase of the film thickness. The electrical properties of the films are investigated. The carrier concentration and Hall mobility both increase with the increase of buffer layer thickness. However, the resistivity reaches the lowest at about 50 nm-thick buffer layer. The lowest resistivity and the maximum Hall mobility are both obtained at 1 wt% Al concentration. But the optical transmittance of all the films is greater than 80% regardless of the buffer layer thickness with A1 concentration lower than 5 wt% in the visible region. 展开更多
关键词 ALUMINUM Buffer layers Electron beams Hall mobility QUARTZ X ray diffraction Zinc oxide
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