A model is proposed for the change in turbulent structure of a round jet in the presence of an acoustic excitation. The excitation is initial amplitude at the jet exit. As these waves propagate downstream they extract energy from the mean flow and transfer it to the random turbulence. This results in an increase in the levels of the turbulence and a resulting increase in the radiated broadband noise. An examination is made of the effect of excitation level and frequency on the jet flow. The numerical procedure allows for radial as well as axial variations in the averaged properties of jet to be calculated. The results indicate that the presence of a finite amplitude instability wave increases the spreading of the jet
Work was carried out as part of an ongoing effort to relate instantaneous large-amplitude features o...
The far-field noise spectra of jet engines show for certain jet configurations and turbine tones a c...
A nonlinear interaction model is used to study sources of sound in jets. The model uses quadratic in...
Jet noise is a major concern in the design of commercial aircraft. Studies by various researchers su...
Experiments on the interaction between a turbulent jet and pure tone sound coming from inside the je...
AbstractExperiment and direct numerical simulation provide compelling evidence that nonlinear wave i...
The location of the noise sources within jet flows, their relative importance to the overall radiate...
Aeroacoustic noise generation in a supersonic round jet is studied to understand in particular the e...
Data from the direct numerical simulation (DNS) of a turbulent, compressible (Mach = 1.92) jet has b...
The behavior of a sound in a jet was investigated. It is verified that the far-field acoustic power ...
Acoustic research related to jet flows has established that sound, by amplifying the naturally occur...
An initial value problem with relevance to jet noise is investigated. A plane parallel jet flow is s...
To investigate the possibility of active control of jet noise, knowledge of the noise generation mec...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
Spectral analysis techniques applied to Lighthill aerodynamic sound equation for unified jet noise t...
Work was carried out as part of an ongoing effort to relate instantaneous large-amplitude features o...
The far-field noise spectra of jet engines show for certain jet configurations and turbine tones a c...
A nonlinear interaction model is used to study sources of sound in jets. The model uses quadratic in...
Jet noise is a major concern in the design of commercial aircraft. Studies by various researchers su...
Experiments on the interaction between a turbulent jet and pure tone sound coming from inside the je...
AbstractExperiment and direct numerical simulation provide compelling evidence that nonlinear wave i...
The location of the noise sources within jet flows, their relative importance to the overall radiate...
Aeroacoustic noise generation in a supersonic round jet is studied to understand in particular the e...
Data from the direct numerical simulation (DNS) of a turbulent, compressible (Mach = 1.92) jet has b...
The behavior of a sound in a jet was investigated. It is verified that the far-field acoustic power ...
Acoustic research related to jet flows has established that sound, by amplifying the naturally occur...
An initial value problem with relevance to jet noise is investigated. A plane parallel jet flow is s...
To investigate the possibility of active control of jet noise, knowledge of the noise generation mec...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
Spectral analysis techniques applied to Lighthill aerodynamic sound equation for unified jet noise t...
Work was carried out as part of an ongoing effort to relate instantaneous large-amplitude features o...
The far-field noise spectra of jet engines show for certain jet configurations and turbine tones a c...
A nonlinear interaction model is used to study sources of sound in jets. The model uses quadratic in...