International Journal of Aeroacoustics

Papers
(The median citation count of International Journal of Aeroacoustics is 1. 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 2020-11-01 to 2024-11-01.)
ArticleCitations
Challenges and opportunities for low noise electric aircraft34
Leading edge serrations for the reduction of aerofoil self-noise at low angle of attack, pre-stall and post-stall conditions13
Design of a single degree of freedom acoustic liner for a fan noise test rig12
Slanted septum and multiple folded cavity liners for broadband sound absorption11
An alternative permeable topology design space for trailing-edge noise attenuation11
Multi-degree-of-freedom liner development: Concept to flight test9
Adaptive RBF with hyperparameter optimisation for aeroacoustic applications8
Fundamental investigation using active plasma control to reduce blade–vortex interaction noise8
A bionic noise reduction strategy on the trailing edge of NACA0018 based on the central composite design method8
A proposed wavy shield for suppression of supersonic jet noise utilizing reflections7
An acoustic liner design methodology based on a statistical source model7
Impedance eduction for uniform and multizone acoustic liners7
Numerical study on edge tone with compressible direct numerical simulation: Sound intensity and jet motion6
Impedance models for single and two degree of freedom linings and correlation with grazing flow duct testing6
High fidelity modeling tools for engine liner design and screening of advanced concepts5
Acoustic optimization design of porous materials on sandwich panel under flow-induced vibration5
The effect of the convective momentum transfer on the acoustic boundary condition of perforated liners with grazing mean flow5
Investigations of three over-the-rotor liner concepts at various technology readiness levels5
Angle-of-attack and Mach number effects on the aeroacoustics of an SD7003 airfoil at Reynolds number 60,0004
A fast 3D-MUSIC method for near-field sound source localization based on the bat algorithm4
Aerodynamic noise from long circular and non-circular cylinders using large eddy simulations4
The effect of doors and cavity on the aerodynamic noise of fuselage nose landing gear4
Systematic validation of the PAAShA shielding prediction method4
Airframe noise predictions using the Ffowcs Williams-Hawkings equation4
Jet noise sources for chevron nozzles in under-expanded condition4
Role of nozzle-exit boundary layer in producing jet noise4
Investigation on aerodynamic noise generated from the simplified high-speed train leading cars4
Simulations of multi-rotor interaction noise at hovering & forward flight conditions4
Acoustic versus aerodynamic installation effects on a generic propeller-driven flying architecture4
Reduction of noise generated by cylinder-airfoil interaction using grooved structures on the upstream cylinder4
Aerodynamic noise from an asymmetric airfoil with perforated extension plates at the trailing edge4
Numerical study on the noise propagation characteristics of rotor in non-uniform downwash flowfield Based on Linearized Euler Equations4
Numerical and experimental analysis of the influence of solidity on rotor aeroacoustics at low Reynolds numbers3
Effect of a pylon on the broadband noise sources of counter-rotating turbomachinery3
Aeroacoustic noise prediction of a vertical axis wind turbine using large eddy simulation3
Boundary element analysis on the fuselage scattering of drone noise3
Examination of air flow characteristics over an open rectangular cavity between the plates3
Prediction of dipole sources and aeroacoustics field for tandem cylinder flow field based on DBEM/hybrid LES3
Liner development at low technology readiness level utilizing the advanced noise control fan3
A modal boundary element method for axisymmetric acoustic problems in an arbitrary uniform mean flow3
Multi-field coupling prediction for improving aeroacoustic performance of muffler based on LES and FW-H acoustic analogy methods3
Advanced analysis of fan noise measurements supported by theoretical source models3
IFAR liner benchmark challenge #1 – DLR impedance eduction of uniform and axially segmented liners and comparison with NASA results3
Experimental investigation of the fluctuating static pressure in a subsonic axisymmetric jet2
Experimental noise reduction (aeroacoustical enhancement) of a large diameter axial flow cooling fan through a reduction in blade tip clearance2
Aeroacoustic characteristics of supersonic offset jets2
Two-point radiation statistics from large-scale turbulent structures within supersonic jets2
Influence of the liner-type treatment on the trailing-edge noise generated by a flat plate2
Acoustic measurements in single-rotor/wing interaction at low disk loading and Reynolds number2
Investigations of thickness effects on the acoustic characteristics of symmetric and asymmetric airfoils2
An introduction to NASA’s broadband acoustic absorbers that resemble natural reeds2
Analysis of vortex structures evolution and aeroacoustic characteristics in the ultra-high-speed elevator ring-gap flow field1
Effect of geometrical parameters and additional mass on the acoustic and vibration control of the bilayer resonant metamaterials1
Further assessment of a time domain impedance boundary condition for the numerical simulation of noise-absorbing materials1
A comparison of in situ and impedance eduction experimental techniques for acoustic liners with grazing flow and high sound pressure level1
Self active cancellation of fan noise1
Computational aeroacoustics of aerofoil leading edge noise using the volume penalization-based immersed boundary methods1
The acoustic performance of a dual Helmholtz resonators system in the presence of a grazing flow1
On the balance between the tonal and broadband noise of isolated propellers1
Phased array microphone measurement of a ducted low-speed axial flow fan at various operating points with the involvement of the acoustically transparent duct technique1
Bayesian optimisation for low-noise aerofoil design with aerodynamic constraints1
Ffowcs Williams – Hawkings analogy for near-field acoustic sources analysis1
Application of LES combined with a wave equation for the simulation of noise induced by a flow past a generic side mirror1
Acoustic wave radiation from a coaxial pipe with partial lining and inner perforated screen1
Acoustic energy balances for sound radiated from duct exit with mean flow1
Subsonic jet noise source location as a function of nozzle exit boundary layer1
The space-time structure of sound produced by stacked rotors in hover using Vold-Kalman filters and proper orthogonal decomposition1
Numerical study of acoustic source localization of rotor using a novel discrete noise analysis strategy1
Numerical and experimental investigation of aerodynamic noise from a cooling fan in a turbulent flow1
Initial boundary layer state of typical model-scale jet nozzles and its impact on noise1
Flow and acoustics in a model rocket flame deflector and deflector cover1
Hydrodynamic sources of the vortex sound in a two-dimensional shear layer1
Investigation of the effects of volume change on flow structure and acoustic in a silencer1
Flow-noise characteristics of turbocharger compressors with rotational balance cuttings1
Research on the influence of check valve on noise performance of variable frequency scroll refrigeration compressor1
Leveraging large eddy simulations to assess noise source imaging of a controlled supersonic jet1
Numerical simulation on the acoustic wave scattering and fluid perturbations inside confined orifice flow1
Effect of 2D ice accretion on turbulent boundary layer and trailing-edge noise1
Data-driven neural networks for source localization and reconstruction using a planar array1
Sound generated by axisymmetric non-plane entropy waves passing through flow contractions1
Modeling, design, and optimization of a dielectric elastomer acoustic liner1
Effect of solidity on aeroacoustic performance of a vertical axis wind turbine using improved delayed detached eddy simulation1
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