Results 11 to 20 of about 4,706 (230)

Single Channel Blind Source Separation for Wind Turbine Aeroacoustics Signals Based on Variational Mode Decomposition

open access: yesIEEE Access, 2018
The acquisition of aeroacoustics signals of wind turbines is of great significance in environmental noise assessment and fault monitoring of blades. The single acoustic sensor is simpler and more flexible than the acoustic sensors array but it lacks ...
Ya'nan Zhang, Shengbo Qi, Lin Zhou
doaj   +1 more source

Numerical and Experimental Investigations of Axial Flow Fan with Bionic Forked Trailing Edge

open access: yesMachines, 2023
To improve the performance of the aerodynamic properties and reduce the aerodynamic noise of an axial flow fan in the outdoor unit of an air conditioner, this study proposed a bionic forked trailing-edge structure inspired by the forked fish caudal fin ...
Zhong Liang   +5 more
doaj   +1 more source

Experimental Investigations on the Possibility to Apply the Corrugated Sheet Metal Used in the Past with Junkers Aircraft to Reduce Noise for Future European Aircraft. Other Noise Reduction Experiments for Future European Aircraft [PDF]

open access: yesINCAS Bulletin, 2018
This paper shows that corrugated skin used in the past with Junkers aircraft to increase the fuselage and wing rigidity can lead to noise reduction for future European aircraft. If the pressure side of wing which is placed above the engine is corrugated,
Constantin SANDU   +4 more
doaj   +1 more source

Effect of Wavy Leading Edges on Airfoil Trailing-Edge Bluntness Noise

open access: yesAerospace, 2023
Among the several noise-generation mechanisms of airfoil self-noise, trailing-edge bluntness noise is an important noise source, which is caused by the vortex shedding at blunt trailing edges.
Yudi Xing   +4 more
doaj   +1 more source

Assessment of the Vortex Feature-Based Vorticity Confinement Method Applied to Rotor Aerodynamics and Aeroacoustics

open access: yesAerospace, 2023
The accurate prediction of helicopter rotor aerodynamics and aeroacoustics using Computational Fluid Dynamics (CFD) techniques still remains a challenge, as the over-dissipation of numerical schemes results in a higher diffusive rate of rotor wake and ...
Jinbin Fu, Yi Yuan, Luigi Vigevano
doaj   +1 more source

Comparison of outflow boundary conditions for subsonic aeroacoustic simulations [PDF]

open access: yes, 2011
Aeroacoustics simulations require much more precise boundary conditions than classical aerodynamics. Two classes of non-reflecting boundary conditions for aeroacoustics are compared in the present work: characteristic analysis based methods and Tam and ...
H. Deniau   +8 more
core   +1 more source

Research progress on analysis and test methods of aircraft panel flutter

open access: yesHangkong gongcheng jinzhan
Aircraft panel flutter is a typical aeroelastic stability problem that occurs during supersonic flight,and is characterized by aerodynamic unilateral effects and significant structural and aerodynamic nonlinearity.
HE Chuanyang   +4 more
doaj   +1 more source

Aeroacoustics research in Europe: The CEAS-ASC report on 2020 & 2021 highlights [PDF]

open access: yes, 2022
The Council of European Aerospace Societies (CEAS) Aeroacoustics Specialists Committee (ASC) supports and promotes the interests of the scientific and industrial aeroacoustics community on a European scale and European aeronautics activities ...
Balázs Nagy, Attila   +2 more
core   +1 more source

Effect of Controlled Muscle Activation in a Unilateral Vocal Fold Polyp Setting on Vocal Fold Vibration

open access: yesApplied Sciences, 2022
Unilateral vocal fold polyps can lead to incomplete glottal closure and irregular vocal fold vibration. Depending on polyp size and resulting dysphonia severity, voice therapy or surgery may be recommended.
Mingjun Ji   +5 more
doaj   +1 more source

Optimization and engineering verification of excitation scheme for aircraft ground vibration test

open access: yesHangkong gongcheng jinzhan
Ground vibration test is an important part of aircraft model development and strength verification. In aircraft ground vibration test,an appropriate excitation scheme can significantly shorten the test's period and improve the accuracy of mode ...
CHEN Haoyu   +3 more
doaj   +1 more source

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