1-07-2

[1-07-2-03] A study on the aerodynamic performance of axial compressor according to blade aspect ratio

*Hyeon-Jun Yang¹, Hyun-Su Kang¹, Youn-Jea Kim² (1. Graduate School of Mechanical Engineering, Sungkyunkwan University, 2. School of Mechanical Engineering, Sungkyunkwan University)

キーワード：Axial compressor, Aspect ratio, Computational Fluid Dynamics, Gas turbine