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The ROTONET prediction system and initial comparisons with far-field acoustics measurements for the XV-15 tilt-rotor aircraftThe NASA Langley Research Center is developing the ROTONET prediction system, a comprehensive computer program for the prediction of full system rotorcraft noise, to provide an analytical tool for estimating the total noise signature of rotorcraft. It contains models of many rotorcraft noise generating mechanisms. NASA is also performing a series of flight tests to provide comprehensive validation data bases for the ROTONET System. A joint NASA/Bell Helicopter Textron Incorporated test of an XV-15 tilt-rotor aircraft is one of several flight test which has been performed. A data base consisting of spectra, noise level time histories, and effective perceived noise levels, incorporating actual meteorological conditions, and tilt-order aircraft flight dynamics, is being produced from this test. The ROTONET prediction system is described, the flight test methodology is explained, and initial comparisons are shown of ROTONET predictions with data from the flight test. EPNL, noise level time history, and narrowband noise spectra comparisons demonstrate the overall capabilities of the prediction system.
Document ID
19900059892
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Golub, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Weir, Donald S.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Acoustics
Meeting Information
Meeting: Vertical Lift Aircraft Design Conference
Location: San Francisco, CA
Country: United States
Start Date: January 17, 1990
End Date: January 19, 1990
Sponsors: NASA, AHS
Accession Number
90A46947
Distribution Limits
Public
Copyright
Other

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