TY - GEN
T1 - Trailing-edge noise prediction using the non-linear disturbance equations
AU - Christiansen, Monica D.
AU - Morris, Philip J.
AU - Brentner, Kenneth S.
PY - 2011
Y1 - 2011
N2 - Currently, the methods available for wind turbine noise prediction are either based on empirical data or require unrealistic computational costs. Although these methods are very valuable, a computationally efficient tool that is based on first principles is needed. The present research proposes a hybrid computational aeroacoustics approach for predicting turbulent-boundary-layer, trailing-edge (TBL-TE) noise. TBL-TE is of interest because it is a dominant source in the total broadband spectrum of wind turbine aerodynamic noise. The proposed method solves the Non-Linear Disturbance Equations (NLDE) for the unsteady flow field in the vicinity of the airfoil trailing edge, reducing computational time. Then, to calculate the noise radiated to a far-field location, the solution from the NLDE is saved and passed to the aeroacoustics propagation code, PSU-WOPWOP. Recent progress with the development of the NLDE flow solver, TANDEM (Turbulence And Noise using the Disturbance Equation Method) is presented. A qualitative assessment of this progress shows promising results. However, the complete noise prediction method is still in the development stage and is not fully validated in this work.
AB - Currently, the methods available for wind turbine noise prediction are either based on empirical data or require unrealistic computational costs. Although these methods are very valuable, a computationally efficient tool that is based on first principles is needed. The present research proposes a hybrid computational aeroacoustics approach for predicting turbulent-boundary-layer, trailing-edge (TBL-TE) noise. TBL-TE is of interest because it is a dominant source in the total broadband spectrum of wind turbine aerodynamic noise. The proposed method solves the Non-Linear Disturbance Equations (NLDE) for the unsteady flow field in the vicinity of the airfoil trailing edge, reducing computational time. Then, to calculate the noise radiated to a far-field location, the solution from the NLDE is saved and passed to the aeroacoustics propagation code, PSU-WOPWOP. Recent progress with the development of the NLDE flow solver, TANDEM (Turbulence And Noise using the Disturbance Equation Method) is presented. A qualitative assessment of this progress shows promising results. However, the complete noise prediction method is still in the development stage and is not fully validated in this work.
UR - http://www.scopus.com/inward/record.url?scp=85088185532&partnerID=8YFLogxK
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U2 - 10.2514/6.2011-2797
DO - 10.2514/6.2011-2797
M3 - Conference contribution
AN - SCOPUS:85088185532
SN - 9781600869433
T3 - 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)
BT - 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)
Y2 - 5 June 2011 through 8 June 2011
ER -