KavukcuogluMSThesis
ris-r-1457
Nrel Phase Vi
Flutter Model 2
Dissertation
M.G.Goman et al (1994) - PII package: Brief description
Hu X Thesis 2013
CFD Basics
Unified Aerodynamic-Acoustic Formulation
Wing Flutter Analysis2
1 PARALLEL COMPUTATIONS OF 3D UNSTEADY COMPRESSIBLE EULER EQUATIONS WITH STRUCTURAL COUPLING Master’s Candidate Zhenyin Li Advisor: Dr. H. U. Akay Department.
Aerodynamic measurement of high-speed base flows Background The separated wake at the base of cylindrical bodies presents a number of challenges to aerodynamic.
