摘要
本文建立了一个用于计算涡流室内各向异性湍流的k-ε湍流模型,结合双色氩离子激光多普勒测速仪的测量结果,利用经过改进的Kiva-Ⅱ程序计算了吊钟型、CometV型及球型等3种典型柴油机涡流室内的空气流动特性,并与部分实验结果进行了比较。研究结果揭示了各涡流室内的空气流动特性,并阐明了涡流室形状的影响规律。
This paper presents a flow model which is composed of an anisotropic k-εturbulence model and a set of governing equations for the transport of mass,momentum and energy.The Kiva-Ⅱcode has been updated by introducing this flow model and widening its applicable scope to swirl chamber diesel engine.By using the experimental data of two-color laser Doppler velocimetry as the boundary conditions,the updated Kiva-Ⅱ code is used to numerically clarify the flow characteristics in the three typical kinds of swirl chamber geometries,that is,the bell type,the Comet V type and the ball type swirl chamber,some numerical results are compared with the LDV measurement.The results obtained clearly show the processes such as the swirl formation and development, the changes of swirl characteristics and swirl number,the changes of turbulent quantity distribution and the gas temperature distribution.The effects of swirl chamber geometry on flow characteristics are then derived.
出处
《燃烧科学与技术》
CAS
CSCD
1996年第4期322-328,共7页
Journal of Combustion Science and Technology
关键词
数值模拟
湍流
涡流室式柴油机
柴油机
Internal combustion engine
Multidimensional numerical modeling
Anisotropic turbulence
Swirl chamber diesel engine
Swirl chamber geometry