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Explore Books on
nozzle efficiency

1-9 of 9 Books

View Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure By Robert S. Jankovsky

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

By Robert S. Jankovsky

View Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle By Karen A. Deere

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle

By Karen A. Deere

View Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft By Jack G. McArdle

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

By Jack G. McArdle

View First NASA/Industry High Speed Research Program Nozzle Symposium By First NASA/Industry High Speed Research Program Nozzle Symposium (1992 Cleveland, Ohio)

First NASA/Industry High Speed Research Program Nozzle Symposium

First NASA/Industry High Speed Research Program Nozzle Symposium

By First NASA/Industry High Speed Research Program Nozzle Symposium (1992 Cleveland, Ohio)

View Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle By David W. Lam

Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle

Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle

By David W. Lam

View Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 By George T. Carson

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20

Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20

By George T. Carson

View Decomposing solid micropropulsion nozzle performance issues By Brian D. Reed

Decomposing solid micropropulsion nozzle performance issues

Decomposing solid micropropulsion nozzle performance issues

By Brian D. Reed

View An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles By Craig A. Hunter

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

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

By Craig A. Hunter

View Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance By John S. Orme

Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance

Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performance

By John S. Orme