A jet propulsion exhaust nozzle particularly useful in multi-engine installations is described. The exhaust nozzle provides high internal/external, thrust-minus-drag, performance for transonic cruise or transonic acceleration as well as improved performance at subsonic and supersonic speeds. A two dimensional wedge/translating shroud at the nozzle exit gives the variable nozzle exit geometry needed to achieve high engine performance over a wide range of throttle power settings.
Two Dimensional Wedge/Translating Shroud Nozzle
1976
18 pages
Report
Keine Angabe
Englisch
Two Dimensional Wedge/Translating Shroud Nozzle
NTIS | 1976
|Two dimensional wedge/translating shroud nozzle
NTRS | 1978
|