A Review of Erosive Burning Models for Solid Propellant Rocket Motors (Spreadsheet)

dc.contributor.authorMacêdo-Gonçalves, Daniel
dc.date.accessioned2024-06-09T15:03:21Z
dc.date.available2024-06-09T15:03:21Z
dc.date.issued2021-07-27 10:13
dc.description.abstractThis 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).
dc.identifier.citationMacêdo-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
dc.identifier.doi10.17862/cranfield.rd.15059649
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/22214
dc.publisherCranfield University
dc.rightsCC BY 4.0
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subject'burning rate'
dc.subject'combustion instabilities'
dc.subject'turbulent boundary layer'
dc.subject'Non-automotive Combustion and Fuel Engineering (incl. Alternative/Renewable Fuels)'
dc.titleA Review of Erosive Burning Models for Solid Propellant Rocket Motors (Spreadsheet)
dc.typeDataset

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