Algorithmic Advances to Increase the Fidelity of Conceptual Hypersonic Mission Design
<p> The contributions of this dissertation increase the fidelity of conceptual hypersonic mission design through the following innovations: 1) the introduction of coupling between the effects of ablation of the thermal protection system (TPS) and flight dynamics, 2) the introduction of rigid b...
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| Language: | EN |
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Purdue University
2018
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| Online Access: | http://pqdtopen.proquest.com/#viewpdf?dispub=10792495 |