Experimental investigation of broadband trailing edge noise from sharp-edged struts
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[1] Michel Roger,et al. Back-scattering correction and further extensions of amiet's trailing-edge noise model. Part 1: theory , 2005 .
[2] J. Williams,et al. Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane , 1970, Journal of Fluid Mechanics.
[3] Michaela Herr,et al. Trailing-Edge Noise Data Quality Assessment for CAA Validation , 2010 .
[4] Martin V. Masek Fink,et al. Experimental Evaluation of Theories for Trailing Edge and Incidence Fluctuation Noise , 1975 .
[5] W. Blake,et al. A Statistical Description of Pressure and Velocity Fields at the Trailing Edges of a Flat Strut , 1975 .
[6] Claudia Kunze,et al. Effect of Trailing Edge Geometry on Vortex Shedding and Acoustic Radiation , 2002 .
[7] F. Fahy,et al. Mechanics of flow-induced sound and vibration , 1989 .
[8] M. S. Howe. Acoustics of Fluid–Structure Interactions: Index , 1998 .
[9] V. M. Tkachenko,et al. Models of a field of pseudoacoustic turbulent wall pressures and experimental data , 1991 .
[10] Michel Roger,et al. Broadband Self Noise from Loaded Fan Blades , 2004 .
[11] A. V. Smolyakov,et al. Calculation of the spectra of pseudosound wall-pressure fluctuations in turbulent boundary layers , 2000 .
[12] D. Chase,et al. Noise Radiated from an Edge in Turbulent Flow , 1975 .
[13] M. S. Howe. Edge-source acoustic Green's function for an airfoil of arbitrary chord, with application to trailing-edge noise , 2001 .
[14] D. Chase. The character of the turbulent wall pressure spectrum at subconvective wavenumbers and a suggested comprehensive model , 1987 .
[15] F. Farassat,et al. A New Time Domain Formulation for Broadband Noise Predictions , 2002 .
[16] T. Brooks,et al. Trailing edge noise prediction from measured surface pressures , 1981 .
[17] Parviz Moin,et al. Prediction of Sound Generated by Complex Flows at Low Mach Numbers , 2010 .
[18] Thomas F. Brooks,et al. Airfoil self-noise and prediction , 1989 .
[19] S. Hambric,et al. Comparison of semi-empirical models for turbulent boundary layer wall pressure spectra , 2009 .
[20] M. S. Howe. Acoustics of fluid-structure interactions , 1998 .
[21] Thomas Carolus,et al. Large-Eddy Simulation and Trailing-Edge Noise Prediction of an Airfoil with Boundary-Layer Tripping , 2009 .
[22] Thierry Maeder,et al. Reduction of Wind Turbine Noise using Optimized Airfoils and Trailing-Edge Serrations , 2008 .
[23] F. Farassat,et al. Broadband Trailing Edge Noise Predictions in the Time Domain. Revised , 2004 .
[24] Christopher K. W. Tam,et al. Experimental Investigation of the Trailing Edge Noise Mechanism , 1978 .
[25] Christopher K. W. Tam,et al. Discrete tones of isolated airfoils , 1974 .
[26] P. Moin,et al. Computation of Trailing-Edge Flow and Noise Using Large-Eddy Simulation , 2000 .
[27] M. Goody. Empirical Spectral Model of Surface Pressure Fluctuations , 2004 .
[28] Con J Doolan,et al. Broadband trailing edge noise from a sharp-edged strut. , 2011, The Journal of the Acoustical Society of America.
[29] Thomas F. Brooks,et al. Scaling of airfoil self-noise using measured flow parameters , 1985 .
[30] K. L. Chandiramani. Diffraction of evanescent waves, with applications to aerodynamically scattered sound and radiation from unbaffled plates , 1974 .
[31] R. Amiet. Noise due to turbulent flow past a trailing edge , 1976 .
[32] D. Chase,et al. Sound Radiated by Turbulent Flow off a Rigid Half-Plane as Obtained from a Wavevector Spectrum of Hydrodynamic Pressure , 1972 .
[33] Laura A. Brooks,et al. On the aeroacoustic tonal noise generation mechanism of a sharp-edged plate. , 2011, The Journal of the Acoustical Society of America.
[34] M. S. Howe. A review of the theory of trailing edge noise , 1978 .
[35] Xavier Gloerfelt,et al. Trailing edge noise from an isolated airfoil at a high Reynolds number , 2009 .
[36] David P. Lockard,et al. The Airframe Noise Reduction Challenge , 2004 .
[37] D. Chase. Modeling the wavevector-frequency spectrum of turbulent boundary layer wall pressure , 1980 .