The Nozzle Acoustic Test Rig (NATR) was developed to provide additional test capabilities at Lewis needed to meet HSR program goals. The NATR is a large f ree-jet facility (free-jet diameter = 53 in.) with a design Mach number of 0.3. It is located inside a geodesic dome, adjacent to the existing Powered Lift Facility (PLF). The NATR allows nozzle concepts to be acoustically assessed for far-field (approximately 50 feet) noise characteristics under conditions simulating forward flight. An ejector concept was identified as a means of supplying the required airflow for this free-jet facility. The primary stream is supplied through a circular array of choked nozzles and the resulting low pressure in the constant, annular- area mixing section c...
The motivation for development of a supersonic business jet (SSBJ) platform lies in its ability to c...
The Boeing/AFOSR Mach-6 Quiet Tunnel has been achieving low-disturbance flow at high Reynolds number...
Modern military aircraft jet engines are designed with variable-geometry nozzles to provide optimal ...
The nozzle acoustic test rig (NATR) was built at NASA Lewis Research Center to support the High Spee...
NASA Lewis Research Center's (LeRC) newly developed Nozzle Acoustic Test Rig (NATR) is a large free-...
A series of three convergent, round-to-rectangular high aspect ratio (HAR) nozzles were designed for...
The Launch Systems Testbed (LST) represents the evolution of vibroacoustics research and development...
This presentation highlights the activities that researchers at the NASA Lewis Research Center (LeRC...
Six coannular plug nozzle configurations having inverted velocity and temperature profiles, and a ba...
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimal ...
NASA and industry partners desire to reintroduce commercial supersonic airliners to the air transpor...
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimum ...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
The following provides a summary for research being conducted by NASA/LaRC and its contractors and g...
An advanced model turbofan (typical of current engine technology) was tested in the NASA Glenn 9 by ...
The motivation for development of a supersonic business jet (SSBJ) platform lies in its ability to c...
The Boeing/AFOSR Mach-6 Quiet Tunnel has been achieving low-disturbance flow at high Reynolds number...
Modern military aircraft jet engines are designed with variable-geometry nozzles to provide optimal ...
The nozzle acoustic test rig (NATR) was built at NASA Lewis Research Center to support the High Spee...
NASA Lewis Research Center's (LeRC) newly developed Nozzle Acoustic Test Rig (NATR) is a large free-...
A series of three convergent, round-to-rectangular high aspect ratio (HAR) nozzles were designed for...
The Launch Systems Testbed (LST) represents the evolution of vibroacoustics research and development...
This presentation highlights the activities that researchers at the NASA Lewis Research Center (LeRC...
Six coannular plug nozzle configurations having inverted velocity and temperature profiles, and a ba...
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimal ...
NASA and industry partners desire to reintroduce commercial supersonic airliners to the air transpor...
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimum ...
Large-Eddy Simulations (LES) of a compressible nozzle/jet configuration have been carried out. Two j...
The following provides a summary for research being conducted by NASA/LaRC and its contractors and g...
An advanced model turbofan (typical of current engine technology) was tested in the NASA Glenn 9 by ...
The motivation for development of a supersonic business jet (SSBJ) platform lies in its ability to c...
The Boeing/AFOSR Mach-6 Quiet Tunnel has been achieving low-disturbance flow at high Reynolds number...
Modern military aircraft jet engines are designed with variable-geometry nozzles to provide optimal ...