How to Apply
Interested in participating in this research project? Contact the professor or graduate student listed below.
Dr. Alex Povitsky (Mechanical Engineering) | email@example.com
Himel Barua | firstname.lastname@example.org
Interaction of shock wave with boundary layer (SWBL) cause possible formation of recirculation zone and larger-scale zone of influence upstream and downstream of the point of the incident shock wave. These aerodynamic phenomena affect the shear and pressure forces acting on the surface, aerodynamic resistance and aerodynamic heating of propulsive systems and supersonic air vehicles. Numerical modeling using ANSYS tools by solving first principles conservation laws will be critical to evaluate SWBL. The project is of interest of Air Force Research Laboratory (AFRL).
Fall 2019 and Spring 2020
aerospace systems, for credit, stem