SUN Yi,GE Ning,SHU Jie.Research on Coupled Throughflow Calculation of Turbofan Engine Low-pressure Parts[J].航空发动机,2018,44(3):26-30
Research on Coupled Throughflow Calculation of Turbofan Engine Low-pressure Parts
DOI:
Key Words:circumferentially averaged  coupled component  component matching  transition section  through flow model  turbofan
Author NameAffiliationE-mail
SUN Yi,GE Ning,SHU Jie College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China myxiaoke@foxmail.com 
Hits: 796
Download times: 861
Abstract:Purpose of this paper is studying influence of component matching and transition geometric parameter on engine overall performance. It is in accordance with parts of a turbofan engine,such as fan,low-pressure turbine,internal and external bypass,mixing section and nozzle. On the basis of circumferentially averaging Navier-Stokes through-flow governing equations,time marching finite volume method was adopted, every component performance calculation parameter along the passage was compared to experiment. The results indicate that, in design point, the max error of characteristic parameters between calculation and experiment data of every section along engine is within 5%. It shows that the throughflow coupling calculation method is able to predicate engine overall performance quickly and improve matching relationship of every part. Therefore, this method is valuable in preliminary design stage of engine.
View Full Text  View/Add Comment  Download reader