Prediction of Vortex Breakdown over Wing Geometries Using Detached-EddySimulation
The formation of vortices and their interaction with the aircraft wing and body is one
the most interesting problems in aerodynamics. These vortices are usually generated
and convected from different parts of the lift providing devices. Their interaction with
the flow field, can case unsteady force and vibration. At some configurations, it can
alter the aerodynamics characteristics of the aircraft by inducing separated regions in
the flow field which causes sudden loss of the lift know as stall condition. Extensive
information about this phenomenon can be obtained through a computer simulation
during the design process in order to provide required data for the efficient design of
the aircraft. In this research, a computer simulation of this problem will be carried out
using an accurate numerical discretization technique.
View Full Project DescriptionAndrew Pollard
Bombardier Aerospace Inc (Toronto, ON)
Engineering
Manufacturing; Transportation and warehousing
Queen's University
Accelerate