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A finite-difference analysis of the nozzle starting process in an expansion tunnel/

Main Author:	Weilmuenster, K. James
Corporate Authors:	United States National Aeronautics and Space Administration, Langley Research Center, United States. National Aeronautics and Space Administration
Format:	Book
Language:	English
Published:	Washington: NASA, 1975
Series:	NASA technical note 8105
Subjects:	Shock tubes Unsteady flow (Aerodynamics) Jet nozzles Finite differences

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