ResearchSpace

Browsing by Subject "T-tail"

Browsing by Subject "T-tail"

Sort by: Order: Results:

  • DLM for T-Tails
    Thumbnail
    Author: Van Zyl, Louwrens H Date: Jun 2007 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 ... Read more
  • Framework for T-tail flutter analysis
    Thumbnail
    Author: Van Zyl, Louwrens H Date: Jun 2011 The flutter analysis of T-tail aircraft poses challenges that are unique to this configuration, including the fact that the unsteady air loads are dependent on the steady load distribution and static deformation of the aircraft. In particular, ... Read more
  • T-tail flutter analysis using Edge
    Thumbnail
    Author: Van Zyl, Louwrens H ; Gledhill, Irvy MA Date: Nov 2011 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 ... Read more