期刊文献+
共找到9篇文章
< 1 >
每页显示 20 50 100
水润滑塑料合金轴承的弹性变形及其影响 被引量:7
1
作者 彭晋民 王家序 +1 位作者 余江波 杨成云 《农业机械学报》 EI CAS CSCD 北大核心 2002年第3期102-105,共4页
从分析水润滑塑料合金轴承在动压条件下的弹性变形入手 ,推导出支承间隙方程式 ,并通过傅立叶级数对压强函数进行展开 ,分析了弹性变形和压强的关系。最终得出动压条件下压强分布函数和弹性变形函数 ,并以此对实际工况的一些现象进行了... 从分析水润滑塑料合金轴承在动压条件下的弹性变形入手 ,推导出支承间隙方程式 ,并通过傅立叶级数对压强函数进行展开 ,分析了弹性变形和压强的关系。最终得出动压条件下压强分布函数和弹性变形函数 ,并以此对实际工况的一些现象进行了解释。 展开更多
关键词 弹性变形 压强 分布函数 水润滑塑料合金轴承 支承间隙方程
下载PDF
Critical Analyses of Order Parameter and Phase Transitions at High Density in Gross-Neveu Model
2
作者 ZHOUBang-Rong 《Communications in Theoretical Physics》 SCIE CAS CSCD 2003年第1X期67-72,共6页
By critical analyses of the order parameter of symmetry breaking, we have researched the phase transitions at high density in D = 2 and D = 3 Gross-Neveu (GN) model and shown that the gap equation obeyed by the dynami... By critical analyses of the order parameter of symmetry breaking, we have researched the phase transitions at high density in D = 2 and D = 3 Gross-Neveu (GN) model and shown that the gap equation obeyed by the dynamical fermion mass has the same effectivenesss as the effective potentials for such analyses of all the second order and some specJal first order phase transitions. In the meantime we also further ironed out a theoretical divergence and proven that in D = 3 GN model a first order phase transition does occur in the case of zero temperature and finite chemical potential. 展开更多
关键词 Gross-Neveu模型 有序参数分析 间隙方程 有效势 高密度 对称恢复 高压 相变
下载PDF
Symmetry Restoring Phase Transitions at High Density in a 4D Nambu-Jona-Lasinio Model with a Single Order Parameter
3
作者 ZHOUBang-Rong 《Communications in Theoretical Physics》 SCIE CAS CSCD 2003年第6X期669-674,共6页
High density phase transitions in a 4-dimensional Nambu-Jona-Lasinio model containing a single symmetry breaking order parameter coming from the fermion-antifermion condensates are researched and expounded by means of... High density phase transitions in a 4-dimensional Nambu-Jona-Lasinio model containing a single symmetry breaking order parameter coming from the fermion-antifermion condensates are researched and expounded by means of both the gap equation and the effective potential approach. The phase transitions are proven to be second-order at a high temperature T; however at T = 0 they are first- or second-order, depending on whether A/m(0), the ratio of the momentum cutoff A in the fermion-loop integrals to the dynamicalfermion mass m(0) at zero temperature, is less than 3.387 or not. The former condition cannot be satisfied in some models. The discussions further show complete effectiveness of the critical analysis based on the gap equation for second order phase transitions including determination of the condition of their occurrence. 展开更多
关键词 Nambu-Jona-Lasinio模 位相转变 单阶参数 高密度对称恢复 有效势 间隙方程
下载PDF
剃齿刀设计理论基础新议
4
作者 杨国令 孟铂 《沈阳黄金学院学报》 1991年第3期66-69,共4页
关键词 剃齿刀 间隙方程 对应点方程
下载PDF
Gap Equations and Effective Potentials at Finite Temperature and Chemical Potential in D—Dimensional Four—Fermion Models
5
作者 ZHOUBang-Rong 《Communications in Theoretical Physics》 SCIE CAS CSCD 2003年第6期663-666,共4页
We have proven the general relations between the gap equations obeyed by dynamical fermion mass and thecorresponding effective potentials at finite temperature and chemical potential in D-dimensional four-fermion inte... We have proven the general relations between the gap equations obeyed by dynamical fermion mass and thecorresponding effective potentials at finite temperature and chemical potential in D-dimensional four-fermion interactionmodels. This gives an easy approach to get effective potentials directly from the gap equations. We find out explicitexpressions for the effective potentials at zero temperature in the cases of D = 2,3, and 4 for practical use. 展开更多
关键词 four-fermion model thermal field theory gap equation effective potential
下载PDF
Numerical Investigation of Tip Clearance Effects in an Axial Transonic Compressor 被引量:9
6
作者 R. Ciorciari A. Lesser +1 位作者 F. Blaim R. Niehuis 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第2期109-119,共11页
Numerical investigations of the Darmstadt transonic single stage compressor (DTC), in the Rotor1-Stator1 configuration, aimed at advancing the understanding of the effect of different rotor tip gaps and transition mod... Numerical investigations of the Darmstadt transonic single stage compressor (DTC), in the Rotor1-Stator1 configuration, aimed at advancing the understanding of the effect of different rotor tip gaps and transition modelling on the blade surfaces are presented. Steady three dimensional Reynolds Averaged Navier Stokes (RANS) simulations were performed to obtain the flow fields for the different configurations at different operating conditions using the RANS-Solver TRACE. The stage geometry and the multi-block structured grid were generated by G3DMESH and a grid sensitivity analysis was conducted. For the clearance gap region, a fully gridded special H-grid was chosen. Comparisons were made between the flow characteristic at design speed, representative for a transonic flow regime, and at 65% speed, representative for a subsonic flow regime. The computations were used to analyse the flow phenomena through the tip clearance region for the different configurations and their impact on the performance of the compressor stage. 展开更多
关键词 Flow in axial compressor surge and stall tip clearance flow multimode transition model.
原文传递
Three-Dimensional Viscous Numerical Simulation of Tip Clearance Flow in Axial-Flow Pump 被引量:4
7
作者 ChangmingYang CichangChen +1 位作者 JinnuoWang QuankaiJi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2003年第3期231-233,共3页
The blade tip clearance flow in axial-flow pump is simulated based on three-dimensional N-S equations, RNG k -e turbulence model, and SIMPLEC algorithm. It shows that numerical results agree well with experiment data ... The blade tip clearance flow in axial-flow pump is simulated based on three-dimensional N-S equations, RNG k -e turbulence model, and SIMPLEC algorithm. It shows that numerical results agree well with experiment data measured by 5-hole probe through validation. Flow fields at the blade tip and velocity distribution at the exit of rotor are analyzed in detail. The numerical results show that the increase in tip clearance reduces hydro-head, especially at small flow rate. Experiment equipment is also introduced. 展开更多
关键词 axial-flow pump numerical computation clearance flow
原文传递
SPECTRAL GAP SOLUTIONS OF THE DISSIPATIVE KIRCHHOFF EQUATION
8
作者 S.PANIZZI 《Chinese Annals of Mathematics,Series B》 SCIE CSCD 2004年第1期73-86,共14页
The author proves that for initial data in a set S ? (H2(?) ∩ H0(?)) × H0(?), 1 1 unbounded in H0(?) × L2(?), the solut... The author proves that for initial data in a set S ? (H2(?) ∩ H0(?)) × H0(?), 1 1 unbounded in H0(?) × L2(?), the solutions of the Cauchy-Dirichlet problem for the 1 dissipative Kirchho? equation Z ?t u ? ν + L 2 | x u|2dx xu + δ?tu = 0 (x ∈ ?, t > 0), ? are global in [0,+∞) and decay exponentially. The functions in S do not satisfy any additional regularity assumption, instead they must satisfy a condition relating their energy with the largest lacuna in their Fourier expansion. The larger is the lacuna the larger is the energy allowed. 展开更多
关键词 Spectral gap solutions Dissipative Kirchhoff equation Lacunae
原文传递
Numerical Investigation & Comparison of a Tandem-Bladed Turbocharger Centrifugal Compressor Stage with Conventional Design
9
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
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部