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

