An exhaust system or nozzle for use in a gas turbine engine is disclosed herein. The exhaust system is adapted to adjust various streams of pressurized air produced by the gas turbine engine to control operation of the gas turbine engine.
Hybrid exhaust nozzle
2019-10-15
Patent
Electronic Resource
English
Vectoring exhaust nozzle technology
AIAA | 1984
|NTIS | 1973
|Improved locomotive exhaust nozzle
Engineering Index Backfile | 1915
|NTRS | 2012
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