The HSBLT Lab at the University of Notre Dame aims to establish reliable computational models for complex aerodynamic phenomena, including boundary-layer transition to turbulence at high speeds. Current research areas include:
- boundary layer receptivity to freestream disturbances
- roughness effects on transition location
- novel methods for efficient, yet reliable, base flow generation
- multimode interactions at hypersonic speeds
We are actively seeking new Ph.D. students. Qualified applicants should send an email to mpeck3@nd.edu with their resume and a brief statement on their research interests.