Numerical Evaluation of the Use of Aluminum Particles for Enhancing Solid Rocket Motor Combustion Stability
The ability to 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 typically necessitates a comprehensive numerical model for...
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| Format: | Article |
| Language: | English |
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MDPI AG
2015-02-01
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| Series: | Energies |
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| Online Access: | http://www.mdpi.com/1996-1073/8/2/1195 |