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FINITE ELEMENT ANALYSIS FOR CHIP FORMATION IN HIGH SPEED TURNING OPERATIONS BY ARBITRARY LAGRANGIAN EULERIAN METHOD 被引量:2
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作者 usama umer XIE Lijing WANG Xibin 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2006年第4期480-482,共3页
A two-dimensional finite element(FE)model for the high speed turning operations when orthogonally machining AISI H13 tool steel at 49HRC using poly crystalline cubic boron nitride(PCBN)is described.An arbitrary Lagran... A two-dimensional finite element(FE)model for the high speed turning operations when orthogonally machining AISI H13 tool steel at 49HRC using poly crystalline cubic boron nitride(PCBN)is described.An arbitrary Lagrangian Eulerian(ALE)method has been adopted which does not need any chip separation criteria as opposed to the traditional Lagrangian approach.Through FE simulations temperature and stresses distributions are presented that could be helpful in predicting tool life and improving process parameters.The results show that high temperatures are generated along the tool rake face as compared to the shear zone temperatures due to high thermal conductivity of PCBN tools. 展开更多
关键词 Chip formation Finite element(FE) Arbitrary Lagrangian Eulerian(ALE)
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基于有限元和光滑粒子流体动力学的硬质工具钢切屑形貌预测方法研究(英文)
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作者 usama umer Jaber Abu QUDEIRI +1 位作者 Mohammad ASHFAQ Abdulrahman AL-AHMARI 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2016年第11期873-885,共13页
目的:获得有效的高精度切屑形貌仿真方法。创新点:通过比较不同切削参数下采用光滑粒子流体动力学模型和有限元模型仿真获得的切屑形貌,证明光滑粒子流体动力学模型可以很好地实现对节状切屑的仿真,而不需要额外的几何或基于网格的切屑... 目的:获得有效的高精度切屑形貌仿真方法。创新点:通过比较不同切削参数下采用光滑粒子流体动力学模型和有限元模型仿真获得的切屑形貌,证明光滑粒子流体动力学模型可以很好地实现对节状切屑的仿真,而不需要额外的几何或基于网格的切屑分离准则。方法:基于有限元和光滑粒子流体动力学的切削形貌仿真方法。结论:通过比较不同切削参数下采用光滑粒子流体动力学模型和有限元模型仿真获得的切屑形貌,证明了基于裂纹形成与扩展理论,采用合理疲劳参数的标准Johnson-Cook模型完全可以实现对节状切屑形成过程的仿真,也即无需采用修正的Johnson-Cook模型。同时证明了有限元模型和光滑粒子流体动力学方法均可满足不同切削速度和进给量条件下的切削力和切屑形貌仿真。 展开更多
关键词 切屑形貌 有限元 光滑粒子流体动力学 淬硬工具钢 锯齿形切屑
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Numerical Investigation & Comparison of a Tandem-Bladed Turbocharger Centrifugal Compressor Stage with Conventional Design
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作者 Syed Noman Danish Shafiq Rehman Qureshi +3 位作者 Abdelrahman EL-Leathy Salah Ud-Din Khan usama umer Ma Chaochen 《Journal of Thermal Science》 SCIE EI CAS CSCD 2014年第6期523-534,共12页
Extensive numerical investigations of the performance and flow structure in an unshrouded tandem-bladed centrifugal compressor are presented in comparison to a conventional compressor.Stage characteristics are explore... Extensive numerical investigations of the performance and flow structure in an unshrouded tandem-bladed centrifugal compressor are presented in comparison to a conventional compressor.Stage characteristics are explored for various tip clearance levels,axial spacings and circumferential clockings.Conventional impeller was modified to tandem-bladed design with no modifications in backsweep angle,meridional gas passage and camber distributions in order to have a true comparison with conventional design.Performance degradation is observed for both the conventional and tandem designs with increase in tip clearance.Linear-equation models for correlating stage characteristics with tip clearance are proposed.Comparing two designs,it is clearly evident that the conventional design shows better performance at moderate flow rates.However;near choke flow,tandem design gives better results primarily because of the increase in throat area.Surge point flow rate also seems to drop for tandem compressor resulting in increased range of operation. 展开更多
关键词 tandem blade conventional compressor INDUCER exducer numerical simulation
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