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A review and update of the NASA aircraft noise prediction program propeller analysis systemThe National Aeronautics and Space Administration (NASA) Aircraft Noise Prediction Program (ANOPP) Propeller Analysis System (PAS) is a set of computational modules for predicting the aerodynamics, performance, and noise of propellers. The ANOPP PAS has the capability to predict noise levels for propeller aircraft certification and produce parametric scaling laws for the adjustment of measured data to reference conditions. A technical overview of the prediction techniques incorporated into the system is presented. The prediction system has been applied to predict the noise signature of a variety of propeller configurations including the effects of propeller angle of attack. A summary of these validation studies is discussed with emphasis being placed on the wind tunnel and flight test programs sponsored by the Federal Aviation Administration (FAA) for the Piper Cherokee Lance aircraft. A number of modifications and improvements have been made to the system and both DEC VAX and IBM-PC versions of the system have been added to the original CDC NOS version.
Document ID
19900027285
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Golub, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Nguyen, L. Cathy
(Planning Research Corp. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1989
Subject Category
Acoustics
Report/Patent Number
SAE PAPER 891032
Accession Number
90A14340
Distribution Limits
Public
Copyright
Other

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