Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle

Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle

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Bibliographic Details
Main Author: Asbury, Scott C
Corporate Authors: United States National Aeronautics and Space Administration, Langley Research Center
Other Authors: Hunter, Craig A
Format: Government Document Book
Language:English
Published: Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, [1999]
Series:NASA technical paper 209093
NASA technical paper 209093
Subjects:
Boundary layer separation
Convergent-divergent nozzles
Flow visualization
Nozzle flow
Oblique shock waves
Wind tunnel nozzles
Wind tunnel tests

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Stanford University

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Call Number: NAS 1.60:209093

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