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Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20

Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20

By George T. Carson

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Publish Date

1984

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service]

Language

eng

Pages

123

Description:

subjectsJet nozzles