Open AccessSpecial aspects of numerical simulation of a two-stage axial-flow compressor with defective blades
Author(s) -
В. Л. Блинов,
И. С. Зубков,
E. Yu. Iskortsev,
O. V. Belyaev,
P. I. Plishkin
Publication year - 2022
Publication title -
vestnik samarskogo universiteta. aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie
Language(s) - English
Resource type - Journals
eISSN - 2541-7533
pISSN - 2542-0453
DOI - 10.18287/2541-7533-2021-20-4-7-19
Subject(s) - gas compressor , axial compressor , airfoil , computational fluid dynamics , stage (stratigraphy) , flow (mathematics) , computer science , basis (linear algebra) , computer simulation , mechanical engineering , structural engineering , mechanics , engineering , simulation , mathematics , geology , physics , geometry , paleontology
The paper presents the results of a stage of development of an analytical model for assessing the impact of various defects on the operation of an axial-flow compressor. Some recommendations on setting the numerical models for carrying out gas dynamic and strength analysis of compressor stages and blades with account for various defects are proposed. Verification was carried out for the models presented: the results are also presented in the paper. On the basis of the verification results some special aspects of CFD-modeling are discussed. The requirements for the defects under investigation are defined. A classification of the defects that can be analyzed with the use of the developed mathematical description of the geometry of airfoils and blades with account of all proposed recommendations for the setting of the numerical model is presented.