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精细线路板面粗糙度分析及验证 被引量:7
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作者 朱拓 刘剑锋 《印制电路信息》 2015年第1期26-30,共5页
线路板进一步向高密度发展,线宽线间距不断缩小,对板面粗糙度的要求也随之提升。文章主要分析了精细线路印制板板面粗糙度原理,并验证了"砂带+不织布"磨板的板面粗糙度效果。实验表明,使用1000#砂带+600#不织布磨板可获得最... 线路板进一步向高密度发展,线宽线间距不断缩小,对板面粗糙度的要求也随之提升。文章主要分析了精细线路印制板板面粗糙度原理,并验证了"砂带+不织布"磨板的板面粗糙度效果。实验表明,使用1000#砂带+600#不织布磨板可获得最佳板面粗糙度,板厚≥1.0mm时,才建议使用此类磨板方法制作。 展开更多
关键词 精细线路 板面粗糙度 砂带磨 不织布磨
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A Study on Modelling Surface Finish in Electrical Discharge Machining Tablet Shape Punches Using Response Surface Methodology
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作者 Le Xuan Hung Tran Thanh Hoang Vu Ngoc Pi 《Journal of Environmental Science and Engineering(B)》 2017年第7期387-390,共4页
This paper introduces a study on modelling surface finish in EDM (Electrical Discharge Machining) of tablet shape punches when using copper as electrode material. In this study, 27 experiments were performed based o... This paper introduces a study on modelling surface finish in EDM (Electrical Discharge Machining) of tablet shape punches when using copper as electrode material. In this study, 27 experiments were performed based on BBD (Box-Behnken Design) and the work-piece material was 9CrSi steel. The input process parameters were the current, the pulse on time, the pulse off time and the voltage. The effects of the input parameters on the surface finish were evaluated by analysing variance. Besides, from the results of the experiments, a regression equation for determining the surface roughness is introduced. Also, the optimum input parameter values were found in order to get the minimum surface roughness. 展开更多
关键词 EDM (Electrical Discharge Machining) EDM sinking surface roughness RSM (Response Surface Methodology) BBD(Box-Behken Design).
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Implementation of a Roughness Element to Trip Transition in Large-eddy Simulation 被引量:2
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作者 J.Boudet J.-F.Monier F.Gao 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第1期30-36,共7页
In aerodynamics, the laminar or turbulent regime of a boundary layer has a strong influence on friction or heat transfer. In practical applications, it is sometimes necessary to trip the transition to turbulent, and a... In aerodynamics, the laminar or turbulent regime of a boundary layer has a strong influence on friction or heat transfer. In practical applications, it is sometimes necessary to trip the transition to turbulent, and a common way is by use of a roughness element (e.g. a step) on the wall. The present paper is concerned with the numerical im- plementation of such a trip in large-eddy simulations. The study is carried out on a flat-plate boundary layer con- figuration, with Reynolds number Rex=l.3x 106. First, this work brings the opportunity to introduce a practical methodology to assess convergence in large-eddy simulations. Second, concerning the trip implementation, a volume source term is proposed and is shown to yield a smoother and faster transition than a grid step. Moreover, it is easier to implement and more adaptable. Finally, two subgrid-scale models are tested: the WALE model of Nic0ud and Ducros (Flow Turbul. Combust., vol. 62, 1999) and the shear-improved Smagorinsky model of Ldv^que et al. (J. Fluid Mech., vol. 570, 2007). Both models allow transition, but the former appears to yield a faster transition and a better prediction of friction in the turbulent regime. 展开更多
关键词 large-eddy simulation boundary layer roughness element TRANSITION TRIPPING
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