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Thermal state of the shell for supersonic part of the ramjet nozzle |
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| Authors: | G P Zarubin V N Zimin G N Kuvyrkin |
| Institution: | 1.Moscow State Technical University,Moscow,Russia |
| Abstract: | A mathematical model describing the temperature distribution in a non-cooled nozzle shell was constructed. Analysis of this model showed that the extreme temperatures are permissible for some modern and promising heat-resistant composite materials. |
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