Results 21 to 30 of about 8,352,814 (137)

The Effects of a Morphed Trailing-Edge Flap on the Aeroacoustic and Aerodynamic Performance of a 30P30N Aerofoil

open access: yesAcoustics, 2022
This paper presents initial results on the aeroacoustic and aerodynamic effects of morphing the trailing-edge flap of the 30P30N aerofoil, over five flap deflections (5–25°), at an 8° angle of attack and a Reynolds number of Re=9.2×105.
Joseph Watkins, Abdessalem Bouferrouk
doaj   +1 more source

Measurement of the Local Sound Pressure on a Bias-Flow Liner Using High-Speed Holography and Tomographic Reconstruction

open access: yesIEEE Access, 2019
Bias-flow liners (BFL) are used as part of the cooling mechanism in airplane turbines and they also enable the reduction of noise emission. The attenuating principle is based on the interaction between sound waves and air flow.
Andres E. Ramos Ruiz   +3 more
doaj   +1 more source

Design of a low-noise aeroacoustic wind tunnel facility at Brunel University [PDF]

open access: yes, 2014
This paper represents the design principle of a quiet, low turbulence and moderately high speed aeroacoustic wind tunnel which was recently commissioned at Brunel University.
Kim, JH   +5 more
core   +1 more source

Performance and Efficiency of Cross-Flow Fans—A Review

open access: yesEnergies, 2023
Cross-Flow Fans (CFFs) have been widely applied in the automotive and domestic air conditioning industries in recent decades. They are high-pressure coefficient turbomachines compacted diametrically, and thus, the complex interactions of these fans ...
Hamid Reza Vanaei   +6 more
doaj   +1 more source

Aeroacoustic performance of a scoop inlet [PDF]

open access: yes4th Aeroacoustics Conference, 1977
A low speed wind tunnel test demonstrated the aerodynamic and acoustic performance of a scoop inlet. Engine noise is directed upward by the extended lower lip of the scoop inlet. In addition, more of the scoop airflow comes in from above the inlet than below, leading to relatively higher surface velocities on the upper lip and lower surface velocities ...
openaire   +1 more source

Assessing the Aeroacoustic Response of a Vehicle to Transient Flow Conditions from the Perspective of a Vehicle Occupant [PDF]

open access: yes, 2014
On-road, a vehicle experiences unsteady flow conditions due to turbulence in the natural wind, moving through the unsteady wakes of other road vehicles and travelling through the stationary wakes generated by roadside obstacles. Separated flow structures
Sims-Williams, D.B.   +5 more
core   +1 more source

Design and performance of an open jet wind tunnel for aero-acoustic measurement [PDF]

open access: yes, 2009
This paper presents the design and performance of an open jet, blow down wind tunnel that was newly commissioned in the anechoic chamber at the ISVR, University of Southampton, UK. This wind tunnel is intended for the measurement of airfoil trailing edge
Chong, T.P.   +5 more
core   +1 more source

Aerodynamic and Aeroacoustic Performance of Serrated Airfoils

open access: yes21st AIAA/CEAS Aeroacoustics Conference, 2015
The aerodynamic and aeroacoustic performance of serrated airfoils have been studied experimentally. A comprehensive aerodynamic study of a symmetric (NACA 0012) and an asymmetric (NACA 65(12)-10) airfoil with different types of trailing-edge serrations has been performed.
Liu, Xiao   +3 more
openaire   +3 more sources

On the aeroacoustic properties of a beveled plate

open access: yesE3S Web of Conferences, 2015
The flow around a beveled flat plate model with an asymmetric 25 degrees trailing edge with three rounding radii is analyzed using a Navier-Stokes based open source software package OpenFOAM in order to predict the aeroacoustic properties of the models ...
van der Velden W.C.P.   +3 more
doaj   +1 more source

Large-Eddy Simulation of the Aerodynamic and Aeroacoustic Performance of a Ventilation Fan [PDF]

open access: yesAdvances in Acoustics and Vibration, 2013
There are controversial requirements involved in developing numerical methodologies in order to compute the flow in industrial fans. The full resolution of turbulence spectrum in such high-Reynolds number flow configurations entails unreasonably expensive computational costs.
BIANCHI, STEFANO   +4 more
openaire   +2 more sources

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