A CFD framework for aeroelastic gust load calculations

dc.contributor.advisorMalan, Arnaud
dc.contributor.authorMan, William Liw Tat
dc.date.accessioned2019-02-08T14:07:43Z
dc.date.available2019-02-08T14:07:43Z
dc.date.issued2018
dc.date.updated2019-02-07T08:30:13Z
dc.description.abstractA Computational Fluid Dynamics (CFD) framework for the simulation of the aeroelastic response of aircraft flying under gust loading was developed. The multiphysics, Finite Volume, VertexCentered code Elementaltextsuperscript{textregistered} was employed and calculations were performed for the transonic flow regime. In the structural domain, the fuselage was treated as rigid and the wing was considered for aeroelastic calculations. The latter was represented by a beam stick model using Timoshenko beam theory in Elementaltextsuperscript{textregistered}'s structural module. The case under consideration was the NASA Common Research Model (CRM) flying at Ma = 0.86 with a 30 ft gust applied over the aircraft. Key contributions of this work included implementation of a computationally efficient gust model as well as the development of a fluidstructure interface. The latter was to transfer forces from a deforming wing skin to the wing-beam in a conservative manner while reflecting the resulting displacements on the wing surface. An interface library was developed for this purpose and 3rd order accurate Bezier curves used to recover a smooth deformed wing. The various sub-components of the aeroelastic model were rigorously validated. Following this, the developed framework was applied to the CRM under gust load conditions.
dc.identifier.apacitationMan, W. L. T. (2018). <i>A CFD framework for aeroelastic gust load calculations</i>. (). University of Cape Town ,Engineering and the Built Environment ,Department of Mechanical Engineering. Retrieved from http://hdl.handle.net/11427/29439en_ZA
dc.identifier.chicagocitationMan, William Liw Tat. <i>"A CFD framework for aeroelastic gust load calculations."</i> ., University of Cape Town ,Engineering and the Built Environment ,Department of Mechanical Engineering, 2018. http://hdl.handle.net/11427/29439en_ZA
dc.identifier.citationMan, W. 2018. A CFD framework for aeroelastic gust load calculations. University of Cape Town.en_ZA
dc.identifier.ris TY - Thesis / Dissertation AU - Man, William Liw Tat AB - A Computational Fluid Dynamics (CFD) framework for the simulation of the aeroelastic response of aircraft flying under gust loading was developed. The multiphysics, Finite Volume, VertexCentered code Elementaltextsuperscript{textregistered} was employed and calculations were performed for the transonic flow regime. In the structural domain, the fuselage was treated as rigid and the wing was considered for aeroelastic calculations. The latter was represented by a beam stick model using Timoshenko beam theory in Elementaltextsuperscript{textregistered}'s structural module. The case under consideration was the NASA Common Research Model (CRM) flying at Ma = 0.86 with a 30 ft gust applied over the aircraft. Key contributions of this work included implementation of a computationally efficient gust model as well as the development of a fluidstructure interface. The latter was to transfer forces from a deforming wing skin to the wing-beam in a conservative manner while reflecting the resulting displacements on the wing surface. An interface library was developed for this purpose and 3rd order accurate Bezier curves used to recover a smooth deformed wing. The various sub-components of the aeroelastic model were rigorously validated. Following this, the developed framework was applied to the CRM under gust load conditions. DA - 2018 DB - OpenUCT DP - University of Cape Town LK - https://open.uct.ac.za PB - University of Cape Town PY - 2018 T1 - A CFD framework for aeroelastic gust load calculations TI - A CFD framework for aeroelastic gust load calculations UR - http://hdl.handle.net/11427/29439 ER - en_ZA
dc.identifier.urihttp://hdl.handle.net/11427/29439
dc.identifier.vancouvercitationMan WLT. A CFD framework for aeroelastic gust load calculations. []. University of Cape Town ,Engineering and the Built Environment ,Department of Mechanical Engineering, 2018 [cited yyyy month dd]. Available from: http://hdl.handle.net/11427/29439en_ZA
dc.language.isoeng
dc.publisher.departmentDepartment of Mechanical Engineering
dc.publisher.facultyFaculty of Engineering and the Built Environment
dc.publisher.institutionUniversity of Cape Town
dc.subject.otherMechanical Engineering
dc.titleA CFD framework for aeroelastic gust load calculations
dc.typeMaster Thesis
dc.type.qualificationlevelMasters
dc.type.qualificationnameMSc
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