Author/Authors :
Devenport، نويسنده , , William J. and Burdisso، نويسنده , , Ricardo A. and Borgoltz، نويسنده , , Aurelien and Ravetta، نويسنده , , Patricio A. and Barone، نويسنده , , Matthew F. and Brown، نويسنده , , Kenneth A. and Morton، نويسنده , , Michael A.، نويسنده ,
Abstract :
The aerodynamic and acoustic performance of an anechoic wind tunnel test section with walls made from thin Kevlar cloth have been measured and analyzed. The Kevlar test section offers some advantages over a conventional free-jet arrangement. The cloth contains the bulk of the flow but permits the transmission of sound with little loss. The containment results in smaller far-field aerodynamic corrections meaning that larger models can be tested at higher Reynolds numbers. The containment also eliminates the need for a jet catcher and allows for a much longer test section. Model-generated noise is thus more easily separated from facility background using beamforming. Measurements and analysis of acoustic and aerodynamic corrections for a Kevlar-walled test section are presented and discussed, along with benchmark trailing edge noise measurements.