International Journal of Aeroacoustics

Papers
(The TQCC of International Journal of Aeroacoustics is 2. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-02-01 to 2025-02-01.)
ArticleCitations
A physics merged deep neural network-based prediction method for jet turbulent mixing noise40
Leading edge serrations for the reduction of aerofoil self-noise at low angle of attack, pre-stall and post-stall conditions15
Fundamental investigation using active plasma control to reduce blade–vortex interaction noise12
SwirlProp: A tool for sound propagation and attenuation in swirling flows11
Experimental noise reduction (aeroacoustical enhancement) of a large diameter axial flow cooling fan through a reduction in blade tip clearance11
Investigations of three over-the-rotor liner concepts at various technology readiness levels11
Flow and acoustics in a model rocket flame deflector and deflector cover9
Editorial8
Guest editor biography8
Guest editor biography8
Experimental investigation of the laminar boundary layer vortex-shedding noise by an airfoil within a closed-vein wind tunnel7
A comparison of tonal-broadband decomposition algorithms for propeller noise7
An improved algorithm for liner impedance eduction in low signal-to-noise ratio flow duct7
Numerical study on the noise propagation characteristics of rotor in non-uniform downwash flowfield Based on Linearized Euler Equations6
Corrigendum to The effect of the convective momentum transfer on the acoustic boundary condition of perforated liners with grazing mean flow6
An introduction to NASA’s broadband acoustic absorbers that resemble natural reeds6
Editorial6
Practical considerations for ray casting shear layer corrections5
Influence of the liner-type treatment on the trailing-edge noise generated by a flat plate5
Effect of solidity on aeroacoustic performance of a vertical axis wind turbine using improved delayed detached eddy simulation5
Guest editor biography5
An acoustic liner design methodology based on a statistical source model5
Guest editor biography5
An alternative permeable topology design space for trailing-edge noise attenuation5
Systematic validation of the PAAShA shielding prediction method5
Supersonic jet noise and screech tone suppression using cross-wire4
Initial boundary layer state of typical model-scale jet nozzles and its impact on noise4
Guest editor biography4
Modeling, design, and optimization of a dielectric elastomer acoustic liner4
Guest editor biographies4
Boundary element analysis on the fuselage scattering of drone noise4
Numerical and experimental investigation of aerodynamic noise from a cooling fan in a turbulent flow4
Reminiscing about Prof. John E. Ffowcs Williams4
Challenges and opportunities for low noise electric aircraft4
Guest editor biography3
Investigations of thickness effects on the acoustic characteristics of symmetric and asymmetric airfoils3
Guest editor biography3
The effect of doors and cavity on the aerodynamic noise of fuselage nose landing gear3
Data-driven neural networks for source localization and reconstruction using a planar array3
Investigation on aerodynamic noise generated from the simplified high-speed train leading cars3
Role of nozzle-exit boundary layer in producing jet noise3
Axisymmetric cavity noise control using passive protrusion3
Comparison and application of the far-field identification algorithms for multiple sound sources based on microphone array2
Aerodynamic noise characteristics of non-circular cylinders in subcritical flow regime2
Aeroacoustic source localization using the microphone array method with application to wind turbine noise2
Christopher Tam: Brief history and accomplishments2
Editorial2
Influence of nozzle external geometry on the emission of screech tones2
Guest editor biography2
Adaptive RBF with hyperparameter optimisation for aeroacoustic applications2
On the balance between the tonal and broadband noise of isolated propellers2
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