A Review of Erosive Burning Models for Solid Propellant Rocket Motors (Spreadsheet)
Date published
2021-07-27 10:13
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Cranfield University
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Citation
Macêdo-Gonçalves, Daniel (2021). A Review of Erosive Burning Models for Solid Propellant Rocket Motors (Spreadsheet). Cranfield Online Research Data (CORD). Dataset. https://doi.org/10.17862/cranfield.rd.15059649
Abstract
This spreadsheet, an integral part of the thesis "A Review of Erosive Burning Models for Solid Propellant Rocket Motors" (Guided Weapon Systems MSc, 2020/2021), presents a useful tool in modelling the erosive burning rate of composite and double-base propellants, from modifications to the theoretical model originally proposed by Paul and Mukunda (1997).
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Keywords
'burning rate', 'combustion instabilities', 'turbulent boundary layer', 'Non-automotive Combustion and Fuel Engineering (incl. Alternative/Renewable Fuels)'
DOI
10.17862/cranfield.rd.15059649
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CC BY 4.0