OOIR: Observatory of International Research

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 2020-05-01 to 2024-05-01.)

Article	Citations
Challenges and opportunities for low noise electric aircraft	20
Leading edge serrations for the reduction of aerofoil self-noise at low angle of attack, pre-stall and post-stall conditions	12
Design of a single degree of freedom acoustic liner for a fan noise test rig	11
Slanted septum and multiple folded cavity liners for broadband sound absorption	10
Wall pressure fluctuations induced by a single stream jet over a semi-finite plate	10
An alternative permeable topology design space for trailing-edge noise attenuation	10
Experimental investigation of porous materials for trailing-edge noise reduction	9
Effects of porous trailing edge on aerodynamic noise characteristics	8
Adaptive RBF with hyperparameter optimisation for aeroacoustic applications	8
A bionic noise reduction strategy on the trailing edge of NACA0018 based on the central composite design method	8
Numerical investigation of porous materials for trailing edge noise reduction	8
On the integration of acoustic phase-gradient metasurfaces in aeronautics	8
Development of 3D boundary element method for the simulation of acoustic metamaterials/metasurfaces in mean flow for aerospace applications	8
Simulations of rocket launch noise suppression with water injection from impingement pad	8
Fundamental investigation using active plasma control to reduce blade–vortex interaction noise	7
Impedance models for single and two degree of freedom linings and correlation with grazing flow duct testing	6
Impedance eduction for uniform and multizone acoustic liners	6
Numerical study on edge tone with compressible direct numerical simulation: Sound intensity and jet motion	6
An acoustic liner design methodology based on a statistical source model	6
Multi-degree-of-freedom liner development: Concept to flight test	5
A proposed wavy shield for suppression of supersonic jet noise utilizing reflections	5
Impedance modelling of acoustically treated circumferential grooves for over-tip-rotor fan noise suppression	5
Jet noise sources for chevron nozzles in under-expanded condition	4
Aerodynamic noise from an asymmetric airfoil with perforated extension plates at the trailing edge	4
Acoustic versus aerodynamic installation effects on a generic propeller-driven flying architecture	4

Aerodynamic noise from long circular and non-circular cylinders using large eddy simulations	4
Investigations of three over-the-rotor liner concepts at various technology readiness levels	4
Airframe noise predictions using the Ffowcs Williams-Hawkings equation	4
Role of nozzle-exit boundary layer in producing jet noise	4
The effect of the convective momentum transfer on the acoustic boundary condition of perforated liners with grazing mean flow	4
Aeroacoustic noise prediction of a vertical axis wind turbine using large eddy simulation	3
Investigation on aerodynamic noise generated from the simplified high-speed train leading cars	3
High fidelity modeling tools for engine liner design and screening of advanced concepts	3
Liner development at low technology readiness level utilizing the advanced noise control fan	3
The effect of doors and cavity on the aerodynamic noise of fuselage nose landing gear	3
Reduction of noise generated by cylinder-airfoil interaction using grooved structures on the upstream cylinder	3
Development of acoustic “meta-liners” providing sub-wavelength absorption	3