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A.H. van Zuijlen
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Computational aeroacoustic analysis of trailing edge noise
A Direct Numerical Simulation using the Lattice Boltzmann Method
To investigate the mechanisms of wing trailing edge noise the aeroacoustic sound generation by a NACA 0018 has been computed with direct numerical simulations using the Lattice Boltzmann Method. Noise from the straight trailing edge wing is compared with the sound generated by a
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