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Title: Experimental investigation of the low speed stall flutter of an airfoil
Author: Li, Jing
ISNI:       0000 0001 2415 8337
Awarding Body: Manchester
Current Institution: University of Manchester
Date of Award: 2007
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Stall flutter is a nonlinear aeroelastic phenomenon that can affect several types of aeroelastic systems such as helicopter rotor blades, wind turbine blades and highly flexible wings. While the related aerodynamic phenomenon of dynamic Stall has been the subject of many experimental studies, stall flutter itself has rarely been Investigated. This thesis presents a set of experiments conducted on a NACA 0012 airfoil undergoing stall flutter oscillations in a low speed wind tunnel.
Supervisor: Not available Sponsor: Not available
Qualification Name: Thesis (Ph.D.) Qualification Level: Doctoral
EThOS ID:  DOI: Not available