Add to ORKGAcoustic and flow characteristics of subsonic and supersonic jets from convergent nozzle
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimal ...
Jet engine noise generation and noise propagation was investigated by studying supersonic nozzle flo...
An experimental investigation was conducted to study and compare the acoustic radiation of air jets ...
Convergent and parallel flow nozzles were used with room temperature air to investigate the flow and...
An experimental investigation of the jet noise radiated to the far field from a 15.2-cm-diam potenti...
The near field fluctuating pressure and aerodynamic mean flow characteristics of a cold subsonic jet...
The aeroacoustic supersonic performance of various internal nozzle geometries is evaluated for shock...
An experimental investigation of a series of four convergent-divergent exhaust nozzles was conducted...
Parameters which contribute to supersonic jet shock noise were investigated for the purpose of deter...
This paper describes a study of sound generated by supersonic jets such as those emanating from the ...
Jet noise on underexpanded supersonic jets are studied with emphasis on determining the role played ...
Both aerodynamic and near field acoustic behavior of several unheated axisymmetric shock free and sh...
AbstractModern military aircraft jet engines are designed with variable-geometry nozzles to provide ...
The results of an experimental study of the acoustic far-field, the shock associated noise, and the ...
The sound pressures radiating from the exhaust streams of two convergent-divergent and one convergen...
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimal ...
Jet engine noise generation and noise propagation was investigated by studying supersonic nozzle flo...
An experimental investigation was conducted to study and compare the acoustic radiation of air jets ...
Convergent and parallel flow nozzles were used with room temperature air to investigate the flow and...
An experimental investigation of the jet noise radiated to the far field from a 15.2-cm-diam potenti...
The near field fluctuating pressure and aerodynamic mean flow characteristics of a cold subsonic jet...
The aeroacoustic supersonic performance of various internal nozzle geometries is evaluated for shock...
An experimental investigation of a series of four convergent-divergent exhaust nozzles was conducted...
Parameters which contribute to supersonic jet shock noise were investigated for the purpose of deter...
This paper describes a study of sound generated by supersonic jets such as those emanating from the ...
Jet noise on underexpanded supersonic jets are studied with emphasis on determining the role played ...
Both aerodynamic and near field acoustic behavior of several unheated axisymmetric shock free and sh...
AbstractModern military aircraft jet engines are designed with variable-geometry nozzles to provide ...
The results of an experimental study of the acoustic far-field, the shock associated noise, and the ...
The sound pressures radiating from the exhaust streams of two convergent-divergent and one convergen...
Modern military aircraft jet engines are designed with variable geometry nozzles to provide optimal ...
Jet engine noise generation and noise propagation was investigated by studying supersonic nozzle flo...
An experimental investigation was conducted to study and compare the acoustic radiation of air jets ...