The paper presents the method for the creation eroded compressor blades and results of the numerical simulation of the transonic axial compressor stage NASA Stage 37 with critical erosion wear. Based on the computational results the method for prediction the influence of the erosion’s intermediate degrees was demonstrated and analyzed. The perspective methods for further stages of the study were noted.
Translated title of the contributionASSESSMENT OF THE EROSION WEAR INFLUENCE ON THE OPERATIONAL PARAMETERS OF THE GAS TURBINE UNIT’S AXIAL COMPRESSOR WITH CFD
Original languageRussian
Pages (from-to)51-60
Number of pages10
JournalПолет. Общероссийский научно-технический журнал
Issue number1-2
Publication statusPublished - 2023

    Level of Research Output

  • VAK List
  • Russian Science Citation Index

ID: 40263248