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XV-15 Low-Noise Terminal Area Operations TestingTest procedures related to XV-15 noise tests conducted by NASA-Langley and Bell Helicopter Textron, Inc. are discussed. The tests. which took place during October and November 1995, near Waxahachie, Texas, documented the noise signature of the XV-15 tilt-rotor aircraft at a wide variety of flight conditions. The stated objectives were to: -provide a comprehensive acoustic database for NASA and U.S. Industry -validate noise prediction methodologies, and -develop and demonstrate low-noise flight profiles. The test consisted of two distinct phases. Phase 1 provided an acoustic database for validating analytical noise prediction techniques; Phase 2 directly measured noise contour information at a broad range of operating profiles, with emphasis on minimizing 'approach' noise. This report is limited to a documentation of the test procedures, flight conditions, microphone locations, meteorological conditions, and test personnel used in the test. The acoustic results are not included.
Document ID
19980047341
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Edwards, B. D.
(Textron Bell Helicopter Fort Worth, TX United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1998
Subject Category
Acoustics
Report/Patent Number
BHTI-690-099-450
NAS 1.26:206946
NASA/CR-1998-206946
Report Number: BHTI-690-099-450
Report Number: NAS 1.26:206946
Report Number: NASA/CR-1998-206946
Funding Number(s)
PROJECT: RTOP 538-07-15-10
CONTRACT_GRANT: NAS1-20094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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