A general solution for the thermal stresses and strains in an infinite, hollow, case-bonded rocket grain
The object of this investigation was to develop a general solution for the thermal stresses and strains in a hollow cylindrical case-bonded solid propellant. The heat conduction equation, as solved by Carslaw and Jaeger, was applied to a hollow composite cylinder. The temperature distribution from...
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| Format: | Others |
| Language: | en |
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Virginia Polytechnic Institute
2020
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| Online Access: | http://hdl.handle.net/10919/101356 |