Christoph Hader
Assistant Research Professor
Laminar-turbulent boundary-layer transition (transonic, supersonic, hypersonic) High Performance Computing Numerical Methods Hypersonic flow Supersonic flow Flow control for low and high-speed flows Transition modelling for Reynolds Averaged Navier-Stokes (RANS) codes Direct Numerical Simulations Nonlinear physical mechanisms relevant for laminar-turbulent boundary-layer transition
Offering Research Opportunities?
Yes
Prerequisite Courses
None
Majors Considered
Aerospace and Mechanical Engineering, Applied Math, Computer Science
Types of Opportunities
Description of Opportunity
No description given
Start Date
January 2020
Primary Department
Affiliated Departments
Research Location
-
Aerospace & Mechanical Engr., 301