An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles

An edition of An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles (1995)

An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles

By Craig A. Hunter

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Publish Date

1995

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Boundary layer equations, Mathematical models, Performance prediction, Compressible flow, Nozzle efficiency, Nozzle flow, Static thrust, Nozzle design, Convergent-divergent nozzles