International Journal of Aeroacoustics

Papers
(The TQCC of International Journal of Aeroacoustics is 3. 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 2020-07-01 to 2024-07-01.)
ArticleCitations
Challenges and opportunities for low noise electric aircraft28
Leading edge serrations for the reduction of aerofoil self-noise at low angle of attack, pre-stall and post-stall conditions12
An alternative permeable topology design space for trailing-edge noise attenuation11
Slanted septum and multiple folded cavity liners for broadband sound absorption11
Design of a single degree of freedom acoustic liner for a fan noise test rig11
Experimental investigation of porous materials for trailing-edge noise reduction10
Development of 3D boundary element method for the simulation of acoustic metamaterials/metasurfaces in mean flow for aerospace applications9
A bionic noise reduction strategy on the trailing edge of NACA0018 based on the central composite design method8
Adaptive RBF with hyperparameter optimisation for aeroacoustic applications8
Multi-degree-of-freedom liner development: Concept to flight test8
On the integration of acoustic phase-gradient metasurfaces in aeronautics8
Numerical investigation of porous materials for trailing edge noise reduction8
A proposed wavy shield for suppression of supersonic jet noise utilizing reflections7
Fundamental investigation using active plasma control to reduce blade–vortex interaction noise7
Impedance eduction for uniform and multizone acoustic liners7
An acoustic liner design methodology based on a statistical source model7
Impedance models for single and two degree of freedom linings and correlation with grazing flow duct testing6
Numerical study on edge tone with compressible direct numerical simulation: Sound intensity and jet motion6
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
Impedance modelling of acoustically treated circumferential grooves for over-tip-rotor fan noise suppression5
Angle-of-attack and Mach number effects on the aeroacoustics of an SD7003 airfoil at Reynolds number 60,0004
High fidelity modeling tools for engine liner design and screening of advanced concepts4
The effect of doors and cavity on the aerodynamic noise of fuselage nose landing gear4
Systematic validation of the PAAShA shielding prediction method4
Acoustic versus aerodynamic installation effects on a generic propeller-driven flying architecture4
Jet noise sources for chevron nozzles in under-expanded condition4
Aerodynamic noise from an asymmetric airfoil with perforated extension plates at the trailing edge4
Simulations of multi-rotor interaction noise at hovering & forward flight conditions4
Airframe noise predictions using the Ffowcs Williams-Hawkings equation4
Aerodynamic noise from long circular and non-circular cylinders using large eddy simulations4
Role of nozzle-exit boundary layer in producing jet noise4
A fast 3D-MUSIC method for near-field sound source localization based on the bat algorithm3
Advanced analysis of fan noise measurements supported by theoretical source models3
Aeroacoustic noise prediction of a vertical axis wind turbine using large eddy simulation3
Investigation on aerodynamic noise generated from the simplified high-speed train leading cars3
Reduction of noise generated by cylinder-airfoil interaction using grooved structures on the upstream cylinder3
IFAR liner benchmark challenge #1 – DLR impedance eduction of uniform and axially segmented liners and comparison with NASA results3
Development of acoustic “meta-liners” providing sub-wavelength absorption3
Numerical study on the noise propagation characteristics of rotor in non-uniform downwash flowfield Based on Linearized Euler Equations3
Effect of a pylon on the broadband noise sources of counter-rotating turbomachinery3
Liner development at low technology readiness level utilizing the advanced noise control fan3
Boundary element analysis on the fuselage scattering of drone noise3
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