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

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:
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596 |a 1 
650 7 |a Boundary layer separation  |2 nasat 
650 7 |a Convergent-divergent nozzles  |2 nasat 
650 7 |a Flow visualization  |2 nasat 
650 7 |a Nozzle flow  |2 nasat 
650 7 |a Oblique shock waves  |2 nasat 
650 7 |a Wind tunnel nozzles  |2 nasat 
650 7 |a Wind tunnel tests  |2 nasat 
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