z-logo
open-access-imgOpen Access
Hot-film measurements of the steady and unsteady boundary layer development on a low-pressure turbine airfoil
Author(s) -
Xue Zhang
Publication year - 2002
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.22215/etd/2002-05208
Subject(s) - airfoil , boundary layer , turbine , materials science , mechanics , aerospace engineering , mechanical engineering , engineering , physics

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom