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 2020-03-01 to 2024-03-01.)
ArticleCitations
Challenges and opportunities for low noise electric aircraft18
Estimation of the lower cut-off frequency of an anechoic chamber: An empirical approach15
Numerical study of 3-D finlets using Reynolds-averaged Navier–Stokes computational fluid dynamics for trailing edge noise reduction14
Leading edge serrations for the reduction of aerofoil self-noise at low angle of attack, pre-stall and post-stall conditions11
Slanted septum and multiple folded cavity liners for broadband sound absorption10
Wall pressure fluctuations induced by a single stream jet over a semi-finite plate10
Design of a single degree of freedom acoustic liner for a fan noise test rig10
An alternative permeable topology design space for trailing-edge noise attenuation9
Adaptive RBF with hyperparameter optimisation for aeroacoustic applications8
Simulations of rocket launch noise suppression with water injection from impingement pad8
A bionic noise reduction strategy on the trailing edge of NACA0018 based on the central composite design method8
Experimental investigation of porous materials for trailing-edge noise reduction8
On the integration of acoustic phase-gradient metasurfaces in aeronautics8
Development of 3D boundary element method for the simulation of acoustic metamaterials/metasurfaces in mean flow for aerospace applications8
Numerical investigation of porous materials for trailing edge noise reduction8
Fundamental investigation using active plasma control to reduce blade–vortex interaction noise7
Effects of porous trailing edge on aerodynamic noise characteristics7
Impedance models for single and two degree of freedom linings and correlation with grazing flow duct testing6
Impedance eduction for uniform and multizone acoustic liners6
Numerical study on edge tone with compressible direct numerical simulation: Sound intensity and jet motion6
A proposed wavy shield for suppression of supersonic jet noise utilizing reflections5
An acoustic liner design methodology based on a statistical source model5
Impedance modelling of acoustically treated circumferential grooves for over-tip-rotor fan noise suppression5
Aerodynamic noise from long circular and non-circular cylinders using large eddy simulations4
The effect of the convective momentum transfer on the acoustic boundary condition of perforated liners with grazing mean flow4
Role of nozzle-exit boundary layer in producing jet noise4
Acoustic versus aerodynamic installation effects on a generic propeller-driven flying architecture4
Multi-degree-of-freedom liner development: Concept to flight test4
Airframe noise predictions using the Ffowcs Williams-Hawkings equation4
Reduction of noise generated by cylinder-airfoil interaction using grooved structures on the upstream cylinder3
Investigation on aerodynamic noise generated from the simplified high-speed train leading cars3
Investigations of three over-the-rotor liner concepts at various technology readiness levels3
Jet noise sources for chevron nozzles in under-expanded condition3
The effect of doors and cavity on the aerodynamic noise of fuselage nose landing gear3
High fidelity modeling tools for engine liner design and screening of advanced concepts3
Development of acoustic “meta-liners” providing sub-wavelength absorption3
Aerodynamic noise from an asymmetric airfoil with perforated extension plates at the trailing edge3
A fast 3D-MUSIC method for near-field sound source localization based on the bat algorithm2
Prediction of dipole sources and aeroacoustics field for tandem cylinder flow field based on DBEM/hybrid LES2
Liner development at low technology readiness level utilizing the advanced noise control fan2
Influence of the liner-type treatment on the trailing-edge noise generated by a flat plate2
Simulations of multi-rotor interaction noise at hovering & forward flight conditions2
Effect of a pylon on the broadband noise sources of counter-rotating turbomachinery2
Advanced analysis of fan noise measurements supported by theoretical source models2
Aeroacoustic noise prediction of a vertical axis wind turbine using large eddy simulation2
An introduction to NASA’s broadband acoustic absorbers that resemble natural reeds2
Diffraction of sound waves by a lined cylindrical cavity2
Experimental investigation of the fluctuating static pressure in a subsonic axisymmetric jet2
Two-point radiation statistics from large-scale turbulent structures within supersonic jets2
Numerical study on the noise propagation characteristics of rotor in non-uniform downwash flowfield Based on Linearized Euler Equations2
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