Browsing by Subject "Aeroelasticity"

Now showing items 1-2 of 2

    • Advanced linear methods for T–tail aeroelasticity 

      Van Zyl, Louwrens Hermias (North-West University, 2011)
      Flutter is one of the primary aeroelastic phenomena that must be considered in aircraft design. Flutter is a self-sustaining structural vibration in which energy is extracted from the air flow and transferred to the ...

    • T-tail flutter: potential-flow modelling,experimental validation and flight tests 

      Murua, Joseba; Van Zyl, Louw; Martinez, Pablo; Climent, Hector; Palacios, Rafael (Elsevier, 2014)
      Flutter of T-tail configurations is caused by the aeroelastic coupling between the vertical fin and the horizontal stabiliser. The latter is mounted on the fin instead of the fuselage, and hence the arrangement presents ...