A Numerical Study of Two-Phase Transonic Steam Flow through Convergence-Divergence Nozzles with Different Rates of Expansion
محل انتشار: هشتمین کنفرانس انجمن هوافضای ایران
سال انتشار: 1388
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 2,102
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شناسه ملی سند علمی:
AEROSPACE08_108
تاریخ نمایه سازی: 5 شهریور 1388
چکیده مقاله:
During the transonic flow of steam in a divergence nozzle, flow first supercools and then nucleates to become a two-phase droplet flow. This phenomenon especially occurs in the last stages of steam turbines and affects the performance. In this research, a numerical scheme for two-phase flow in nozzle passages is developed. An Eulerian Eulerian reference frame is used for both phases. The Shear Stress Transport turbulence model is used to model the Reynolds stresses appeared in the averaged Navier-Stokes equations. The SIMPLE algorithm is used to solve the discritized equations and a homogenous nucleation model applied for the mass transfer in the transonic conditions. In this paper three nozzles with different rate of expansion are employed to be under study. Overall (static to total); pressure ratio and droplet size through the results are compared with the experimental data and good agreements are observed. Also, the two-phase results are compared with the dry steam simulation in the same pressure condition and the differences of pressure and Mach profiles for these types are the case of discussion.
کلیدواژه ها:
نویسندگان
Behnam Nikkhahi
MSc Student, Faculty of Mech. Engn., K.N.Toosi University of Technology, Iran
Mehrzad Shams
Associated Professor. Faculty of Mech. Engn., K.N.Toosi University of Technology, Iran
Masoud Ziabasharhagh
Assistant Professor, Faculty of Mech. Engn., K.N.Toosi University of Technology, Iran