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DLM for T-Tails

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dc.contributor.author Van Zyl, Louwrens H
dc.date.accessioned 2009-03-04T12:10:16Z
dc.date.available 2009-03-04T12:10:16Z
dc.date.issued 2007-06
dc.identifier.citation Van Zyl, L.H. 2007. DLM for T-Tails. International Forum on Aeroelasticity and Structural Dynamics. Stockholm, Sweden, June, pp 15. en
dc.identifier.uri http://hdl.handle.net/10204/3117
dc.description International Forum on Aeroelasticity and Structural Dynamics. Stockholm, Sweden, June 2007 en
dc.description.abstract This paper describes the extension of the DLM to account for effects that are critical to the modelling of T-tail flutter. The boundary condition is made more general to account for yaw/dihedral and sideslip/dihedral coupling and the calculation of forces is generalised to account for lateral load due to roll, and rolling moment due to yaw, yaw rate and sideslip. In addition, the steady load and the quadratic components of the mode shapes are taken into account in the calculation of generalised forces en
dc.language.iso en en
dc.subject T-tail en
dc.subject Subsonic unsteady aerodynamics en
dc.subject Doublet lattice method en
dc.title DLM for T-Tails en
dc.type Conference Presentation en
dc.identifier.apacitation Van Zyl, L. H. (2007). DLM for T-Tails. http://hdl.handle.net/10204/3117 en_ZA
dc.identifier.chicagocitation Van Zyl, Louwrens H. "DLM for T-Tails." (2007): http://hdl.handle.net/10204/3117 en_ZA
dc.identifier.vancouvercitation Van Zyl LH, DLM for T-Tails; 2007. http://hdl.handle.net/10204/3117 . en_ZA
dc.identifier.ris TY - Conference Presentation AU - Van Zyl, Louwrens H AB - This paper describes the extension of the DLM to account for effects that are critical to the modelling of T-tail flutter. The boundary condition is made more general to account for yaw/dihedral and sideslip/dihedral coupling and the calculation of forces is generalised to account for lateral load due to roll, and rolling moment due to yaw, yaw rate and sideslip. In addition, the steady load and the quadratic components of the mode shapes are taken into account in the calculation of generalised forces DA - 2007-06 DB - ResearchSpace DP - CSIR KW - T-tail KW - Subsonic unsteady aerodynamics KW - Doublet lattice method LK - https://researchspace.csir.co.za PY - 2007 T1 - DLM for T-Tails TI - DLM for T-Tails UR - http://hdl.handle.net/10204/3117 ER - en_ZA


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