Scale Effects on Solid Rocket Combustion Instability Behaviour

The ability to understand and predict the expected internal behaviour of a given solid-propellant rocket motor under transient conditions is important. Research towards predicting and quantifying undesirable transient axial combustion instability symptoms necessitates a comprehensive numerical model...

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Bibliographic Details
Main Author: David R. Greatrix
Format: Article
Language:English
Published: MDPI AG 2011-01-01
Series:Energies
Subjects:
Online Access:http://www.mdpi.com/1996-1073/4/1/90/