Van Zyl, Louwrens H2009-03-042009-03-042007-06Van Zyl, L.H. 2007. DLM for T-Tails. International Forum on Aeroelasticity and Structural Dynamics. Stockholm, Sweden, June, pp 15.http://hdl.handle.net/10204/3117International Forum on Aeroelasticity and Structural Dynamics. Stockholm, Sweden, June 2007This 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 forcesenT-tailSubsonic unsteady aerodynamicsDoublet lattice methodConference PresentationVan Zyl, L. H. (2007). DLM for T-Tails. http://hdl.handle.net/10204/3117Van Zyl, Louwrens H. "DLM for T-Tails." (2007): http://hdl.handle.net/10204/3117Van Zyl LH, DLM for T-Tails; 2007. http://hdl.handle.net/10204/3117 .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 -