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Converging nozzle design for a subsonic wind tunnel to test heat sinks under impinging and parallel airflows

No description available.
Identiferoai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/17124
Date05 1900
CreatorsSzleper, Michele Lee
PublisherGeorgia Institute of Technology
Source SetsGeorgia Tech Electronic Thesis and Dissertation Archive
Detected LanguageEnglish
TypeThesis
RightsAccess restricted to authorized Georgia Tech users only.

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