Nozzle Efficiency

10 books
Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressureRobert S. Jankovsky

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

Robert S. Jankovsky

1996No page data
First NASA/Industry High Speed Research Program Nozzle SymposiumFirst 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 (1992 Cleveland, Ohio)

1999No page data
Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20George T. Carson
⏱ 2h 51m

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

George T. Carson

1988171 pp.
Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzleKaren A. Deere

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

Karen A. Deere

1999No page data
Decomposing solid micropropulsion nozzle performance issuesBrian D. Reed

Decomposing solid micropropulsion nozzle performance issues

Brian D. Reed

2003No page data
Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzleDavid W. Lam

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

David W. Lam

1995No page data
An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzlesCraig A. Hunter

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

Craig A. Hunter

1995No page data
Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraftJack G. McArdle
⏱ 14m

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

Jack G. McArdle

199014 pp.
Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurationsKevin L. Mikkelsen

Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations

Kevin L. Mikkelsen

2001No page data
Initial flight test evaluation of the F-15 ACTIVE axisymmetric vectoring nozzle performanceJohn S. Orme

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

John S. Orme

1998No page data