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 |