NASA NTRS · 19750000242
Computer program for the attenuation of high bypass turbofan engine noise
Abstract
Two computer programs determine effect of boundary layer on attenuation of sound in a circular duct lined with material used in noise suppresion in fan inlet and exhaust ducts of turbofan engines.
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Veldman, H. F.. 1975-10-01. Computer program for the attenuation of high bypass turbofan engine noise. https://ntrs.nasa.gov/citations/19750000242
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