Acoustic research related to jet flows has established that sound, by amplifying the naturally occuring large-scale structures in turbulent shear layers, can cause a more rapidly decay of the jet plume velocity and temperature and an increase in jet spreading rate. One possible application of this sound-flow interaction phenomenon is to future STOL aircraft that may require modified jet plume characteristics in order to reduce the loads and temperatures on the deflected flaps during take-off and landing operations. The tone-excitation effect on the velocity decay of model-scale, two-stream jet plumes is analyzed. Measured data are correlated in terms of parameters that include excitation sound level and outer-to-inner stream velocity ratio....
AbstractResults from recent LES studies of high-speed jet flows and its near and far-field noise (Me...
The second part of a three-part report on the effects of acoustic excitation on jet mixing includes ...
Current research programs directed at supersonic engine exhaust noise reduction are demonstrating be...
Noise from an unheated sonic jet in the presence of an external flow is measured in a free-jet wind ...
A model is proposed for the change in turbulent structure of a round jet in the presence of an acous...
Mean plume static and pitot pressures and far-field acoustic pressure were measured for an underexpa...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
The behavior of a sound in a jet was investigated. It is verified that the far-field acoustic power ...
Aircraft noise mitigation is an ongoing challenge for the aeronautics research community. In respons...
When a jet is closely installed under a solid surface, turbulent jet plume is modified. Two levels o...
The location of the noise sources within jet flows, their relative importance to the overall radiate...
AbstractResults from recent LES studies of high-speed jet flows and its near and far-field noise (Me...
Noise sources in high-speed jets were identified by directly correlating flow density fluctuation (c...
Experiments on the interaction between a turbulent jet and pure tone sound coming from inside the je...
Some of the background to contemporary jet aeroacoustics is addressed. Then scaling laws for noise g...
AbstractResults from recent LES studies of high-speed jet flows and its near and far-field noise (Me...
The second part of a three-part report on the effects of acoustic excitation on jet mixing includes ...
Current research programs directed at supersonic engine exhaust noise reduction are demonstrating be...
Noise from an unheated sonic jet in the presence of an external flow is measured in a free-jet wind ...
A model is proposed for the change in turbulent structure of a round jet in the presence of an acous...
Mean plume static and pitot pressures and far-field acoustic pressure were measured for an underexpa...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
The behavior of a sound in a jet was investigated. It is verified that the far-field acoustic power ...
Aircraft noise mitigation is an ongoing challenge for the aeronautics research community. In respons...
When a jet is closely installed under a solid surface, turbulent jet plume is modified. Two levels o...
The location of the noise sources within jet flows, their relative importance to the overall radiate...
AbstractResults from recent LES studies of high-speed jet flows and its near and far-field noise (Me...
Noise sources in high-speed jets were identified by directly correlating flow density fluctuation (c...
Experiments on the interaction between a turbulent jet and pure tone sound coming from inside the je...
Some of the background to contemporary jet aeroacoustics is addressed. Then scaling laws for noise g...
AbstractResults from recent LES studies of high-speed jet flows and its near and far-field noise (Me...
The second part of a three-part report on the effects of acoustic excitation on jet mixing includes ...
Current research programs directed at supersonic engine exhaust noise reduction are demonstrating be...