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?


Prerequisite Courses


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