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Modelling of supersonic combustion


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.

Research location

Aerospace, Mechanical and Mechatronic Engineering

Program type




Additional information

Scholarships available for exceptional applicants.

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Opportunity ID

The opportunity ID for this research opportunity is 2810

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