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Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to mach 2.01/

Main Author:	Maiden, Donald L.
Corporate Authors:	United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: NASA, 1975
Series:	NASA technical note 7906
Subjects:	Jet nozzles > Testing Aerodynamics, Supersonic

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