Theoretical and numerical modelling of nozzle erosion on hybrid rockets and development of numerical algorithms allowing for self-consistent simulations

To study into detail the thermo mechanical behavior of a nozzle throat in order to finally develop a numerical algorithm to be implemented on CFD simulation to perfrom self-consisten simulation of nozzle-erosion; Development of analytical model;Validation versus literature data.

Research Fields

Engineering

Other costs

social security contributions

Selection process

comparative assessment of qualifications, scientic and professional curriculum, scientific productivity and INTERVIEW


Programme Description
Number of awards per year1
Annual budget25177
Eligible destination country/ies for fellowsItaly
Eligibility of fellows: country/ies of residenceInternational
Eligibility of fellows: nationality/iesInternational
Website of Fellowship Programmehttp://www.dii.unipd.it
Fellowship's Details
Career StageExperienced researcher or 4-10 yrs (Post-Doc)
Research ProfilesNot defined
Employment contract with full social securityyes
Total amount per fellowship per year25177
Currencyeuro
Covers salaryyes
Maximum duration of fellowship12

Application deadline

26/02/2015