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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Format: | Article |
Language: | English |
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MDPI AG
2011-01-01
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Series: | Energies |
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Online Access: | http://www.mdpi.com/1996-1073/4/1/90/ |