
Investigating the Impact of Using CFD Generated Unsteady Mach Number Dynamic Stall Data for Numerical Rotor Analysis of Helicopter Forward Flight
Author(s) -
Dustin Jee
Publication year - 2018
Language(s) - English
Resource type - Dissertations/theses
DOI - 10.22215/etd/2017-12184
Subject(s) - stall (fluid mechanics) , freestream , computational fluid dynamics , aerodynamics , mach number , pitching moment , aerospace engineering , engineering , computer science , mechanics , angle of attack , physics , turbulence , reynolds number