Tip clearance flow-shock interaction in an advanced, transonic, axial-flow compressor rotor

Author

Steven Lee Puterbaugh, University of Dayton

Date of Award

1994

Degree Name

Ph.D. in Mechanical Engineering

Keywords

Compressors Aerodynamics, Axial flow compressors, Aircraft gas-turbines Blades, Gas-turbines Blades, Gas-turbines Aerodynamics

Rights Statement

Copyright © 1994, author

Recommended Citation

Puterbaugh, Steven Lee, "Tip clearance flow-shock interaction in an advanced, transonic, axial-flow compressor rotor" (1994). Graduate Theses and Dissertations. 5048.
https://ecommons.udayton.edu/graduate_theses/5048