Numerical simulation of three-dimensional turbulent flow in multistage axial compressor blade row

Abstract

Numerical simulation of three-dimensional turbulent flow in a multistage axial compressor blade row is conducted. A high resolution, third-order ENN scheme is adopted to catch the shockwave and simulate the turbulent flow correctly,

Keywords

multistage axial compressor / numerical simulation / high order accuracy and high resolution scheme / implicit method / treatment for rotor-stator interactional surface