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  • 1
    Publication Date: 2016-06-07
    Description: Noise can be predicted by solving Full (time-dependent) Compressible Navier-Stokes Equation (FCNSE) with computational domain. The fluctuating near field of the jet produces propagating pressure waves that produce far-field sound. The fluctuating flow field as a function of time is needed in order to calculate sound from first principles. Noise can be predicted by solving the full, time-dependent, compressible Navier-Stokes equations with the computational domain extended to far field - but this is not feasible as indicated above. At high Reynolds number of technological interest turbulence has large range of scales. Direct numerical simulations (DNS) can not capture the small scales of turbulence. The large scales are more efficient than the small scales in radiating sound. The emphasize is thus on calculating sound radiated by large scales.
    Keywords: Acoustics
    Type: First NASA/Industry High Speed Research Program Nozzle Symposium; 25-1 - 25-7; NASA/CP-1999-209423
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-10
    Description: A numerical analysis of the shock-sound interaction problem is presented, using quasi-1-D Euler equations.
    Keywords: Acoustics
    Type: Third Computational Aeroacoustics (CAA) Workshop on Benchmark Problems; 33-40; NASA/CP-2000-209790
    Format: text
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