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Users' manual for the Langley high speed propeller noise prediction program (DFP-ATP)The use of the Dunn-Farassat-Padula Advanced Technology Propeller (DFP-ATP) noise prediction program which computes the periodic acoustic pressure signature and spectrum generated by propellers moving with supersonic helical tip speeds is described. The program has the capacity of predicting noise produced by a single-rotation propeller (SRP) or a counter-rotation propeller (CRP) system with steady or unsteady blade loading. The computational method is based on two theoretical formulations developed by Farassat. One formulation is appropriate for subsonic sources, and the other for transonic or supersonic sources. Detailed descriptions of user input, program output, and two test cases are presented, as well as brief discussions of the theoretical formulations and computational algorithms employed.
Document ID
19890005449
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dunn, M. H.
(Planning Research Corp. Hampton, VA, United States)
Tarkenton, G. M.
(Planning Research Corp. Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Publication Information
Publisher: NASA
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:4208
NASA-CR-4208
Report Number: NAS 1.26:4208
Report Number: NASA-CR-4208
Accession Number
89N14820
Funding Number(s)
CONTRACT_GRANT: NAS1-18000
PROJECT: RTOP 535-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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