Open AccessThree-dimensional interaction of a swept shock wave with a turbulent boundary layer and the effects of air injection on separation.
Author(s) -
D. J. Peake
Publication year - 2018
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.22215/etd/1975-00296
Subject(s) - boundary layer , separation (statistics) , flow separation , shock wave , mechanics , turbulence , shock (circulatory) , materials science , meteorology , aerospace engineering , physics , geology , medicine , mathematics , engineering , statistics