太原理工大学学报Issue(1)：49-54,6.DOI:10.16355/j.cnki.issn1007-9432tyut.2015.01.010
超音速射流流场湍流模型适应性研究
Study on Adaptability of Supersonic Jet Flow Turbulence Model
摘要
Abstract
To study and analyze the adaptability of five kinds of turbulence model coming with fluent for supersonic jet systematically ,the five kinds of turbulence model were used for Mach 1.7 nozzle on numerical simulation ,the distribution of velocity and temperature along axial direction was obtained ,and compared with experimentally measured values .The comparative results show that :the results acquired using standard k_εmodel and the standard k_ωmodel ,compared with ex_perimental results ,have big deviation ,w hile the deviation is much smaller w hen using RNG k_εmodel ,realizable k_εmodel and SST k_ωmodel .The comparison with experimental results both in the near field and far field ,shows that the simulation result achieved by SST k_ωmodel simulation has the highest degree in accordance with experimental results ,so the final conclusion was a_chieved:SST k_ωsimulation model is most suitable for the jet simulation for Mach 1.7 nozzle .关键词
湍流模型/超音速射流/SST k_ω模型/流场特性/数值模拟Key words
turbulence models/supersonic jet/SST k_ωsimulation model/field behavior/nu_merical simulation分类
数理科学引用本文复制引用
朱伶枫,张延玲,朱荣,赵飞,田冬东..超音速射流流场湍流模型适应性研究[J].太原理工大学学报,2015,(1):49-54,6.基金项目
国家重大科学仪器设备开发专项基金资助项目 （）
