This PhD project will look at the development, validation and application of computational models for the supersonic combustion. The successful candidate will work with novel physical models and opensource computational codes to study problems that could include shocks and detonations, transitional mixing and primary instabilities.
Associate Professor Matthew Cleary.
Aerospace, Mechanical and Mechatronic Engineering
PHD
N/A
Scholarships available for exceptional applicants.
The opportunity ID for this research opportunity is 2810