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

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1. http://hdl.handle.net/1853/17124
2. 629509

Identifer	oai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/17124
Date	05 1900
Creators	Szleper, Michele Lee
Publisher	Georgia Institute of Technology
Source Sets	Georgia Tech Electronic Thesis and Dissertation Archive
Detected Language	English
Type	Thesis
Rights	Access restricted to authorized Georgia Tech users only.