Effect of Aerodynamic Interaction of Tip Leakage Flow and Secondary Flow on the Performance and Stability of a Transonic Axial Compressor

Files

01_title page.pdf (241.42 KB)

02_preliminary pages.pdf (1.02 MB)

03_chapter_1.pdf (1.07 MB)

04_chapter_2.pdf (938.96 KB)

05_chapter_3.pdf (204.86 KB)

Abstract

Available

URI

http://hdl.handle.net/10603/609599

Collections

Department of Aerospace Engineering