Development of a One and Two-Dimensional Model for Calculating Pore Pressure in an Ablating Thermal Sacrificial Liner
Understanding the behavior of charring or decomposing materials exposed to high temperature environments is an essential aspect in rocket design. In particular, the tip of re-entry vehicles and sacrificial rocket nozzle liners are both exposed to extremely high temperatures. This thesis is specifica...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/42438 http://scholar.lib.vt.edu/theses/available/etd-05032007-114117/ |