Open AccessNumerical and experimental study on the ability of dynamic roughness to alter the development of a leading edge vortex
Author(s) -
Christopher Griffin
Publication year - 2019
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.33915/etd.320
Subject(s) - stall (fluid mechanics) , airfoil , leading edge , aerospace engineering , angle of attack , aerodynamics , wing , vortex lift , pitching moment , vortex , flow separation , engineering , mechanics , boundary layer , lift coefficient , physics , reynolds number , turbulence