Results 21 to 30 of about 11,859 (310)
When the aircraft opens the bay door to let the landing gear either drop or retract, the incoming flow will result in a significant amount of coupling noise from the bay and the landing gear.
Kun Zhao +4 more
doaj +1 more source
Investigation of flow structures involved in sound generation by two- and three-dimensional cavity flows [PDF]
Proper Orthogonal Decomposition and Stochastic Estimation are combined to shed some light on the link between organized flow structures and noise generation by turbulent flows.
DRUAULT, Philippe +5 more
core +1 more source
Turbulent boundary layer noise : direct radiation at Mach number 0.5 [PDF]
Boundary layers constitute a fundamental source of aerodynamic noise. A turbulent boundary layer over a plane wall can provide an indirect contribution to the noise by exciting the structure, and a direct noise contribution.
GLOERFELT, Xavier, BERLAND, Julien
core +1 more source
Design of portable multi-channel high precision acquisition system based on FPGA
In order to meet the high-speed, parallel and high-precision data acquisition of the multi-point sensitive pressure sensor signals on the surface of the rotor blade, and with the functions of program-controlled gain amplification and anti-aliasing ...
Wang Wei +3 more
doaj +1 more source
Effects of Shear Layer Characteristics on Acoustic Propagation and Source Localization
The shear layer characteristics of an open-jet acoustic wind tunnel are of key importance on measurements of aeroacoustics. The effects of thickness, spreading angle and strength of shear layer on acoustic propagation and source localization are ...
doaj +1 more source
Trailing Edge Noise Reduction by Passive and Active Flow Controls [PDF]
This paper presents the results on the use of porous metal foams (passive control) and dielectric barrier surface plasma actuations (active control) for the reduction of vortex shedding tonal noises from the nonflat plate type trailing edge serration in ...
Kim, JH +7 more
core +1 more source
Analysis of Flow Field Structure Characteristics of Dual Impinging Jets at Different Velocities
The flow structure and unsteady evolution characteristics of dual impinging jets represent a flow problem of significant engineering importance in the aerospace field.
Yifan Zhao +5 more
doaj +1 more source
PREDICTION AND VALIDATION FOR THE AERODYNAMIC NOISE OF HIGH-SPEED TRAIN POWER CAR [PDF]
The aerodynamic noise of high-speed train power car was investigated in this article. The full-scale power car was first modeled, and the external steady flow field was computed by a realizable k-ε turbulence model.
Shi-jie JIANG +3 more
doaj +1 more source
To improve the accuracy of the wind tunnel test, relying on the high-pressure gas source of the China Aerodynamic Research and Development Center, a secondary flow standard facility based on a sonic nozzle array was developed, with a pressure range of (1~
Zhihao Zhang +3 more
doaj +1 more source
A method has been developed for predicting the aerodynamic noise from the bogie of a high-speed train using a two-dimensional microphone array in a low-noise wind tunnel.
Nobuhiro YAMAZAKI +5 more
doaj +1 more source

