000			nam a22 7a 4500
999			_c2680 _d2680
003			OSt
005			20170106161907.0
008			170106b xxu||||| |||| 00| 0 eng d
040			_cNational Acoustics Laboratories
245			_aStatistical estimation of trailing edge noise from finite wall-mounted airfoils
520	3		_aIt is important to be able to accurately model the flow and noise generated by finite wall-mounted airfoil flows because of the many engineering applications in which these flows occur. One method for predicting turbulent trailing edge noise is the Reynolds-averaged Navier-Stokes based statistical noise model (RSNM) of Doolan et al. (Proceedings of 20th International Congress on Acoustics, ICA 2010). The RSNM method has previously been used successfully on a range of two-dimensional geometry-flow cases. In this paper a new turbulent velocity cross-spectrum model and improved implementation are proposed to allow the RSNM method to be used to effectively and efficiently predict turbulent trailing edge noise from more complex three-dimensional cases. Reynolds-averaged Navier-Stokes (RANS) simulations of a series of wing-in-junction cases are used in combination with the developed acoustic model to predict the far-field noise and compared against experimental noise measurements.
700			_aJesse Coombs
773	0		_gProceedings 9-11 November 2016, Brisbane, Australia _tAcoustics 2016
856			_uhttp://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/540/p39.pdf?sequence=3&isAllowed=y
942			_2udc _cARTICLE