Investigation of an aeroelastic model for a generic wing structure

Investigation of an aeroelastic model for a generic wing structure

Thesis (MScEng)--Stellenbosch University, 2013. === ENGLISH ABSTRACT: Computational Aeroelasticity is a complex research field which combines structural and aerodynamic analyses to describe a vehicle in flight. This thesis investigates the feasibility of including such an analysis in the developme...

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Bibliographic Details
Main Author: Cilliers, M. E.
Other Authors: Jones, T.
Format: Others
Language:en_ZA
Published: Stellenbosch : Stellenbosch University 2013
Subjects:
Computational aeroelasticity
Structural analysis algorithm
Aerodynamic algorithm
Clark-Y airfoil
Prandtl’s lifting line theory
Dissertations > Electronic engineering
Theses > Electronic engineering
Unmanned aerial vehicles
Drone aircraft
Online Access:http://hdl.handle.net/10019.1/80317

Internet

http://hdl.handle.net/10019.1/80317

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