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An investigation of a method of aircraft control by shock wave interference

No description available.
Identiferoai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/13377
Date12 1900
CreatorsAldridge, Edward Cleveland
PublisherGeorgia Institute of Technology
Source SetsGeorgia Tech Electronic Thesis and Dissertation Archive
Languageen_US
Detected LanguageEnglish
TypeThesis
Format241 bytes, text/html
RightsAccess restricted to authorized Georgia Tech users only.

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