期刊文献+

船舶侧向进气装置一体化数值研究 被引量:4

NUMERICAL RESEARCH ON INTEGRATION OF SHIPPING LATERAL AIR INTAKE DEVICE
原文传递
导出
摘要 不同于以往孤立研究船舶进气装置的研究方法,本文采用三维数值模拟方法结合标准κ-ε模型对侧向进气装置内外流场进行了一体化数值研究。获得了侧向进气装置行驶过程中的气动参数分布以及进气室内部气流分布形态,得出气动损失最大位置,并通过定义总压恢复系数计算了船舶在行驶过程中的阻力分布。 Different from the past isolated research approach on the shipping air intake device, three-dimensional numerical simulation method and normal model were used to research on the integration of inner and outer flow field of the lateral air intake device. Aerodynamic parameters distribution of it and flow field structures in the air intake device were obtained during the process of sailing. The results also show the location for the aerodynamic loss and the drag distribution of the ship by the definition of total-pressure recovery coefficient.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2010年第3期399-402,共4页 Journal of Engineering Thermophysics
关键词 进气装置 侧向 一体化 数值模拟 air intake device lateral integration numerical simulation method
  • 相关文献

参考文献5

二级参考文献10

  • 1吉桂明,李汇文.船舶燃气轮机技术和应用的展望[J].舰船科学技术,2000,22(5):36-40. 被引量:15
  • 2鲍国华.风沿特种实验[M].西安:西北工业大学出版社,1990..
  • 3Alan D O, Stephen D H. More Efficient Applications for Naval Gas Turbines-Addressing the Mismatch between Available Technology and the Requirements of Modern Naval Gas Turbines Inlets. ASME GT2006-90305. 2006.
  • 4Mustapha A C, Cyrus B M H, Thomas Mee III. Inlet Fogging of Gas Turbine Engines: ExperimentM and Analytical Investigations on Impaction Pin Fog Nozzle Behavior. Transactions of the ASME, 2006, 128:826-839.
  • 5Joachim K. Effects of Inlet Flow Distortion on the Performance of Aircraft Gas Turbines. ASME GT2006-90419, 2006.
  • 6孙晓颖,许伟,武越.钝体绕流中的计算域设置研究.见:第十三界全国结构风工程学术会议论文集(下册).2007.1036-1041.
  • 7[1]Marine propulsion 1999-2000 specifications.Gas Turbine World,1999.19:43 ~ 46.
  • 8[2]Fulton K.Marine WR-21 succeeds in 500-hour ICR production engine test program.Gas Turbine World,1997,27(6):22~26.
  • 9[3]Gas Turbine Power for Gruisers.Diesel & Gas Turbine Worldwide,1998,30(6):38 ~ 39.
  • 10楚武利,朱俊强.风速及风向对舰用燃气轮机进气流量的影响[J].燃气轮机技术,2000,13(1):33-37. 被引量:8

共引文献32

同被引文献26

引证文献4

二级引证文献3

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部