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T-tail flutter analysis using Edge

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dc.contributor.author Van Zyl, Louwrens H
dc.contributor.author Gledhill, Irvy MA
dc.date.accessioned 2012-05-03T10:33:02Z
dc.date.available 2012-05-03T10:33:02Z
dc.date.issued 2011-11
dc.identifier.citation Van Zyl, L.J. and Gledhill, I. T-tail flutter analysis using Edge. Edge Conference, Kista, Sweden, November 2011 en_US
dc.identifier.uri http://hdl.handle.net/10204/5830
dc.description Edge Conference, Kista, Sweden, November 2011 en_US
dc.description.abstract A grid was generated with the base of the fin, i.e. the hinge line, on the axis of a cylindrical domain with a diameter of 2m. Due to the axial symmetry of the setup, rotation of the T-tail should not change the pressure distribution on the T-tail. In reality, due to some a-symmetry in the grid, this was not quite achieved. The analyses consisted of a steady solution, followed by a prescribed, sine-squared, disturbance of 0.03 radians (corresponding to 10 mm lateral displacement at the fin top), followed by a coupled time-domain simulation. en_US
dc.language.iso en en_US
dc.relation.ispartofseries Workflow;8517
dc.subject T-tail en_US
dc.subject Flutter en_US
dc.subject Edge en_US
dc.title T-tail flutter analysis using Edge en_US
dc.type Conference Presentation en_US
dc.identifier.apacitation Van Zyl, L. H., & Gledhill, I. M. (2011). T-tail flutter analysis using Edge. http://hdl.handle.net/10204/5830 en_ZA
dc.identifier.chicagocitation Van Zyl, Louwrens H, and Irvy MA Gledhill. "T-tail flutter analysis using Edge." (2011): http://hdl.handle.net/10204/5830 en_ZA
dc.identifier.vancouvercitation Van Zyl LH, Gledhill IM, T-tail flutter analysis using Edge; 2011. http://hdl.handle.net/10204/5830 . en_ZA
dc.identifier.ris TY - Conference Presentation AU - Van Zyl, Louwrens H AU - Gledhill, Irvy MA AB - A grid was generated with the base of the fin, i.e. the hinge line, on the axis of a cylindrical domain with a diameter of 2m. Due to the axial symmetry of the setup, rotation of the T-tail should not change the pressure distribution on the T-tail. In reality, due to some a-symmetry in the grid, this was not quite achieved. The analyses consisted of a steady solution, followed by a prescribed, sine-squared, disturbance of 0.03 radians (corresponding to 10 mm lateral displacement at the fin top), followed by a coupled time-domain simulation. DA - 2011-11 DB - ResearchSpace DP - CSIR KW - T-tail KW - Flutter KW - Edge LK - https://researchspace.csir.co.za PY - 2011 T1 - T-tail flutter analysis using Edge TI - T-tail flutter analysis using Edge UR - http://hdl.handle.net/10204/5830 ER - en_ZA


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