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
Reference:
Van Zyl, L.H. 2007. DLM for T-Tails. International Forum on Aeroelasticity and Structural Dynamics. Stockholm, Sweden, June, pp 15.
Van Zyl, L. H. (2007). DLM for T-Tails. http://hdl.handle.net/10204/3117
Van Zyl, Louwrens H. "DLM for T-Tails." (2007): http://hdl.handle.net/10204/3117
Van Zyl LH, DLM for T-Tails; 2007. http://hdl.handle.net/10204/3117 .
