In this thesis work a physics-based model to predict nozzle thermochemical erosion is presented. This model is based on non-charring materials ablation phenomena and can be used to predict the erosion in the peculiar hybrid rocket motor environment and comparing different propellant compositions
Numerical Investigation of Nozzle Thermochemical Behaviour in Hybrid Rocket Motors
Ruffin, Alessandro
2015/2016
Abstract
In this thesis work a physics-based model to predict nozzle thermochemical erosion is presented. This model is based on non-charring materials ablation phenomena and can be used to predict the erosion in the peculiar hybrid rocket motor environment and comparing different propellant compositionsFile in questo prodotto:
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Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/19430