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Aircraft Noise Prediction Program (ANOPP) Fan Noise Prediction for Small Engines

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:24:06Z
date available2017-09-04T16:24:06Z
date copyright01/01/1996
date issued1996
identifier otherTUHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/87437
description abstractThe Fan Noise Module of ANOPP is used to predict the broadband noise and pure tones for axial flow compressors or fans. The module, based on the method developed by M. F. Heidmann, uses empirical functions to predict fan noise spectra as a function of frequency and polar directivity. Previous studies have determined the need to modify the module to better correlate measurements of fan noise from engines in the 3000To 6000-pound thrust class. Additional measurements made by AlliedSignal have confirmed the need to revise the ANOPP fan noise method for smaller engines. This report describes the revisions to the fan noise method which have been verified with measured data from three separate AlliedSignal fan engines. Comparisons of the revised prediction show a significant improvement in overall and spectral noise predictions.
languageEnglish
titleNASA-CR-198300num
titleAircraft Noise Prediction Program (ANOPP) Fan Noise Prediction for Small Enginesen
typestandard
page186
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1996
contenttypefulltext
subject keywordsAERODYNAMIC NOISE
subject keywordsDATA ACQUISITION
subject keywordsJET ENGINES
subject keywordsNOISE PREDICTION (AIRCRAFT)
subject keywordsNOISE REDUCTION
subject keywordsNOISE SPECTRA
subject keywordsTURBOFANS


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