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An investigation of a method for determining the pressure distribution on an accelerating flat plate at an angle of attack at hypersonic or supersonic velocities

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1. http://hdl.handle.net/1853/12231
2. 109067

Identifer	oai:union.ndltd.org:GATECH/oai:smartech.gatech.edu:1853/12231
Date	08 1900
Creators	Hannon, Clarence William
Publisher	Georgia Institute of Technology
Source Sets	Georgia Tech Electronic Thesis and Dissertation Archive
Language	en_US
Detected Language	English
Type	Thesis
Format	241 bytes, text/html
Rights	Access restricted to authorized Georgia Tech users only.