A NUMERICAL SIMULATION METHOD OF FLOW CHARACTERISTIC FOR A SUBSONIC SINGLE ROTOR AXIAL COMPRESSOR

摘要

Computational processing of the turboengine performance is laborious because now the assessment of real behavior for many of its parts is achieved through its functions characteristic aquired experimentaly. Although they have good results, the theoretical models are insufficient in the design stage of propulsion systems. The present article aims at producing a computational processing of experimental data we have and then to using these results into a quantitative study of flow characteristic of any subsonic axial compressor.