نتایج جستجو برای: aerodynamic noise

تعداد نتایج: 205620  

Journal: :Proceedings. Mathematical, physical, and engineering sciences 2017
Rozhin Hajian Justin W Jaworski

This theoretical study determines the aerodynamic loads on an aerofoil with a prescribed porosity distribution in a steady incompressible flow. A Darcy porosity condition on the aerofoil surface furnishes a Fredholm integral equation for the pressure distribution, which is solved exactly and generally as a Riemann-Hilbert problem provided that the porosity distribution is Hölder-continuous. The...

2015
E. Latorre Iglesias D. J. Thompson M. G. Smith

Vortex shedding from cylinders has been extensively studied due to its occurrence in many engineering fields. Many experimental studies reported in the literature focus on the aerodynamics of the vortex shedding process but the literature about the radiated noise is more scarce. The aim of the work presented here is to extend the available noise data. Aero-acoustic wind tunnel tests were carrie...

2013
J. Y. Zhu Z. W. Hu D. J. Thompson

As one of the main aerodynamic noise sources of high-speed trains, the bogie is a complex structure containing many components and the flow around it is extremely dynamic with high-level turbulence. Flow around a simplified bogie at scale 1:10 is studied numerically using Computational Fluid Dynamics (CFD) for comparison with experimental measurements. The upstream inlet flow is represented as ...

2015
Cédric Gendrot Barbara Kühnert Didier Demolin

The study of realization of French uvular /ʁ/ is usually considered as problematic due to its variability. In this study, an articulatory (EMA) and aerodynamic experiment allowed us to determine its major axes of variation. We show that the degree of constriction between the tongue and the palate is related to the voicing of the consonant and we validate the use of a harmonic-to-noise ratio for...

1995
Anthony A. Giunta Vladimir Balabanov Susan Burgee Bernard Grossman Raphael T. Haftka William H. Mason

The use of multidisciplinary optimization techniques in aerospace vehicle design often is limited because of the signi cant computational expense incurred in the analysis of the vehicle and its many systems In response to this di culty a variable complexity modeling approach involving the use of re ned and computationally expensive models together with simple and computationally inexpensive mod...

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