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Hypersonic aerospace vehicle leading edge cooling using heat pipe, transpiration and film cooling techniques

No description available.
Identiferoai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/16347
Date08 1900
CreatorsModlin, James Michael
PublisherGeorgia Institute of Technology
Source SetsGeorgia Tech Electronic Thesis and Dissertation Archive
Detected LanguageEnglish
TypeDissertation
RightsAccess restricted to authorized Georgia Tech users only.

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