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

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

by Scott C. Asbury

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First published: 1999 1 language
Subjects
Wind tunnel nozzles Oblique shock waves Flow visualization Boundary layer separation Nozzle flow Wind tunnel tests Convergent-divergent nozzles

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