Add to ORKGPerformance of aerodynamically positioned auxiliary inlet ejector nozzle at Mach numbers from 0 to 2.
A series of two-dimensional plug nozzles was tested with and without ejector shrouds at free stream ...
Experimental investigations were conducted to determine the aerodynamic performance and noise genera...
Plug nozzles with two types of 40-spoke noise suppressor were tested at free-stream Mach numbers fro...
Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraf
Performance of auxiliary inlet ejector nozzle with floating inlet doors and floating single hinge tr...
Performance of auxiliary inlet ejector nozzle with fixed inlet doors and triple-hinge trailing edge ...
Auxiliary inlet ejector nozzle with fixed doors and single-hinge trailing-edge flap
Flight performance of auxiliary inlet ejector and plug nozzle at transonic speed
Simulated take-off, transonic acceleration, and supersonic flight conditions using auxiliary inlet e...
Fixed geometry wind tunnel model of auxiliary inlet ejector with clamshell flow diverter from Mach 0...
The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height ...
Wind tunnel model tests were conducted to demonstrate the aerodynamic performance improvements of a ...
Flap and nacelle geometry effects on conical plug nozzle performance at subsonic and supersonic velo...
Static tests of nozzle efficiency and pumping characteristics of conical turbojet plug nozzle with t...
The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height ...
A series of two-dimensional plug nozzles was tested with and without ejector shrouds at free stream ...
Experimental investigations were conducted to determine the aerodynamic performance and noise genera...
Plug nozzles with two types of 40-spoke noise suppressor were tested at free-stream Mach numbers fro...
Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraf
Performance of auxiliary inlet ejector nozzle with floating inlet doors and floating single hinge tr...
Performance of auxiliary inlet ejector nozzle with fixed inlet doors and triple-hinge trailing edge ...
Auxiliary inlet ejector nozzle with fixed doors and single-hinge trailing-edge flap
Flight performance of auxiliary inlet ejector and plug nozzle at transonic speed
Simulated take-off, transonic acceleration, and supersonic flight conditions using auxiliary inlet e...
Fixed geometry wind tunnel model of auxiliary inlet ejector with clamshell flow diverter from Mach 0...
The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height ...
Wind tunnel model tests were conducted to demonstrate the aerodynamic performance improvements of a ...
Flap and nacelle geometry effects on conical plug nozzle performance at subsonic and supersonic velo...
Static tests of nozzle efficiency and pumping characteristics of conical turbojet plug nozzle with t...
The results indicated increases in auxiliary-inlet pressure recovery with increases in scoop height ...
A series of two-dimensional plug nozzles was tested with and without ejector shrouds at free stream ...
Experimental investigations were conducted to determine the aerodynamic performance and noise genera...
Plug nozzles with two types of 40-spoke noise suppressor were tested at free-stream Mach numbers fro...