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Experimental aerodynaics characteristics for a cylindrical body of vevolution with side strakes and various noses at angles of attack from O to 58 and mach numbers from 0.6 to 2.0

By: Lel.
Contributor(s): H. Jorgenson.
Material type: materialTypeLabelBookPublisher: Subject(s): Us National Aeronautics And Space AdministrationDDC classification: TR | TMX-3130
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