Add to ORKGPerformance of 10 deg conical turbojet plug nozzle with iris primary and translating shroud for supersonic cruise application
The off-design operation of an isentropic plug nozzle designed for a jet pressure ratio of 15 was in...
The Langley 16-Foot Transonic Tunnel was used to evaluate the performance characteristics of a coann...
Flight test investigation of effects of variable geometry plug nozzles installed on f-106b aircraf
Static tests of nozzle efficiency and pumping characteristics of conical turbojet plug nozzle with t...
Flap and nacelle geometry effects on conical plug nozzle performance at subsonic and supersonic velo...
Cold flow tests of aerodynamic characteristics of plug nozzle configuration for turbojet engines ope...
Performance characteristics of truncated, conical plug nozzle with cylindrical outer shrou
Several variations of a boattailed shroud for a 10 deg conical plug nozzle were tested using an F-10...
Low angle conical plug nozzle with stowed thrust reverser performance at Mach 0 to 2.
Plug and shroud geometry variables on plug nozzle performance at transonic speed
Effects of shroud geometry on performance of collapsible plug nozzle at Mach numbers from 0 to 2.
An experimental investigation was conducted in a nozzle static test facility to determine the perfor...
Effect of plug base contour on performance of fully truncated plug nozzle with translating shrou
An investigation was conducted in the 8- by 6-foot supersonic wind tunnel on the external and intern...
The effects of various afterbody changes on the base pressure of a nacelle-type isentropic plug nozz...
The off-design operation of an isentropic plug nozzle designed for a jet pressure ratio of 15 was in...
The Langley 16-Foot Transonic Tunnel was used to evaluate the performance characteristics of a coann...
Flight test investigation of effects of variable geometry plug nozzles installed on f-106b aircraf
Static tests of nozzle efficiency and pumping characteristics of conical turbojet plug nozzle with t...
Flap and nacelle geometry effects on conical plug nozzle performance at subsonic and supersonic velo...
Cold flow tests of aerodynamic characteristics of plug nozzle configuration for turbojet engines ope...
Performance characteristics of truncated, conical plug nozzle with cylindrical outer shrou
Several variations of a boattailed shroud for a 10 deg conical plug nozzle were tested using an F-10...
Low angle conical plug nozzle with stowed thrust reverser performance at Mach 0 to 2.
Plug and shroud geometry variables on plug nozzle performance at transonic speed
Effects of shroud geometry on performance of collapsible plug nozzle at Mach numbers from 0 to 2.
An experimental investigation was conducted in a nozzle static test facility to determine the perfor...
Effect of plug base contour on performance of fully truncated plug nozzle with translating shrou
An investigation was conducted in the 8- by 6-foot supersonic wind tunnel on the external and intern...
The effects of various afterbody changes on the base pressure of a nacelle-type isentropic plug nozz...
The off-design operation of an isentropic plug nozzle designed for a jet pressure ratio of 15 was in...
The Langley 16-Foot Transonic Tunnel was used to evaluate the performance characteristics of a coann...
Flight test investigation of effects of variable geometry plug nozzles installed on f-106b aircraf