Novel Mathematical Methods for Aerospace and Space Physics Simulation
Postdoctoral fellow: Dr. Lee Betchen
Lead faculty member: Dr. Hans De Sterck
Novel methods for the computationally efficient simulation of compressible fluid flow will be developed, with applications to aerospace and space physics. First, new formulations of multigrid techniques for the implicit solution of time-dependent flows will be studied, using parabolization to increase diagonal dominance and solution efficiency. Second, new direct solution methods for steady transonic flows will be developed, employing dynamical systems and characteristic analysis.
Efficient Numerical Methods for the Time Integration of Unsteady Fluid Flows
Raymond Spiteri , University of Saskatchewan
Multi-scale Adaptive Modelling and Numerical Methods for Reactive Flows
Dr. Clinton P.T. Groth , University of Toronto
This research project looks to develop computer programs which will enable the study of reactive flows and combustion processes in gas turbine engines. Combustion is inherently a multi-scale process that involves a wide range of complicated physical/chemical phenomena, as well as a wide range of spatial and temporal scales.
