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瓦楞纸板楞形参数对力学性能的影响 被引量:4
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作者 宋卫生 薛阳 +1 位作者 边文慧 孙艳美 《包装工程》 CAS 北大核心 2020年第17期147-151,共5页
目的研究瓦楞纸板楞形参数对力学性能的影响规律,以达到在保证力学性能的基础上,减少材料的使用,降低生产成本。方法在国标规定的范围内,均匀选取了瓦楞纸板的楞宽、楞高以及楞峰半径的实验值,设计单因素实验,推导出芯纸压缩比系数公式... 目的研究瓦楞纸板楞形参数对力学性能的影响规律,以达到在保证力学性能的基础上,减少材料的使用,降低生产成本。方法在国标规定的范围内,均匀选取了瓦楞纸板的楞宽、楞高以及楞峰半径的实验值,设计单因素实验,推导出芯纸压缩比系数公式。利用有限元方法进行准静态压缩试验,得出瓦楞纸板的边压强度以及边压强度与压缩比系数的比值。结果压缩比系数随楞宽和楞峰半径的增加逐渐降低,随楞高的增加逐渐增高,楞宽的影响程度最大,其次是楞高,楞峰半径最小;边压强度随楞宽的增加逐渐降低,随楞高的增加整体趋势为逐渐增高,边压强度随楞峰半径的增加,其变化波动较大,在楞峰半径为1.3 mm时边压强度最大。边压强度与压缩比系数的比值在单因素变化的情况下,楞宽为3.4 mm时最大,楞高为3.75 mm时最大,楞峰半径为1.3 mm时最大。结论瓦楞几何参数对瓦楞纸板的边压强度和压缩比系数均有明显的影响,所以选择合适的几何参数组合可以在保证强度的基础上降低材料的使用量。 展开更多
关键词 瓦楞纸板 楞形 几何参数 压缩比系数 边压强度
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Economy of Energy during Refrigerating Machine Operation
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作者 Aleksandr Vasserman Aleksey Slyn'ko 《Journal of Mechanics Engineering and Automation》 2016年第5期265-268,共4页
Idealized cycles of refrigerating machines with adiabatic and isothermal compression of refrigerant vapor were investigated. Energetic characteristics of cycles: specific mass and volume cooling capacity q0 and qv, w... Idealized cycles of refrigerating machines with adiabatic and isothermal compression of refrigerant vapor were investigated. Energetic characteristics of cycles: specific mass and volume cooling capacity q0 and qv, work of compression 1, refrigerating coefficient of performance e and power N for drive of compressor were compared. These characteristics were calculated for eight refrigerants at temperature of their condensation 30 ℃ and temperatures of boiling -15℃ and -30 ℃. The calculations show that the use of isothermal compression of refrigerant vapor ensures economy of energy during refrigerating machine operation. 展开更多
关键词 Vapor compressor refrigerating machines adiabatic and isothermal compression of refrigerant energetic characteristics of cycles.
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Study for the Gas Flow through a Critical Nozzle
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作者 Jae-Hyung Kim Heuy-Dong Kim +1 位作者 Shigeru Matsuo Toshiaki Setoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2003年第3期250-254,259,共6页
In the present study, computational work using the axisymmetric, compressible, Navier-Stokes equations is carried out to predict the discharge coefficient and critical pressure ratio of gas flow through a critical noz... In the present study, computational work using the axisymmetric, compressible, Navier-Stokes equations is carried out to predict the discharge coefficient and critical pressure ratio of gas flow through a critical nozzle. The Reynolds number effects are investigated with several nozzles with different throat diameter. Diffuser angle is varied to investigate the effects on the discharge coefficient and critical pressure ratio. The computational results are compared with the previous experimental ones. It is known that the discharge coefficient and critical pressure ratio are given by functions of the Reynolds number and boundary layer integral properties. It is also found that diffuser angle affects the critical pressure ratio. 展开更多
关键词 compressible flow CHOKE boundary layer critical pressure ratio discharge coefficient
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