Numerical simulation of the structural response of a composite rocket nozzle during the ignition transient.
The following dissertation describes an investigation of the structural response behaviour of a composite solid rocket motor nozzle subjected to thermal and pressure loading during the motor ignition period, derived on the basis of a multidisciplinary numerical simulation approach. To provide quanti...
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| Language: | en |
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2010
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| Online Access: | http://hdl.handle.net/10413/778 |