NASA NTRS · 19780019178
Two dimensional wedge/translating shroud nozzle
Abstract
A jet propulsion exhaust nozzle is reported for multi-engine installations which produces 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 provides the variable nozzle exit geometry needed to achieve high engine performance over a wide range of throttle power settings.
Keep this discovery
Explore connections, maps & timelines
Maiden, D. L.. 1978-05-09. Two dimensional wedge/translating shroud nozzle. https://ntrs.nasa.gov/citations/19780019178
Cite the original work for its findings. Save a collection to share your selection of sources.