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Advanced Study for Active Noise Control in Aircraft (ASANCA)Aircraft interior noise and vibration measurements are included in this paper from ground and flight tests. In addition, related initial noise calculations with and without active noise control are conducted. The results obtained to date indicate that active noise control may be an effective means for reducing the critical low frequency aircraft noise.
Document ID
19920023712
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Borchers, Ingo U. (Dornier Luftfahrt G.m.b.H. Friedrichshafen, Germany)
Emborg, Urban (Saab Aircraft Co. Linkoping, Sweden)
Sollo, Antonio (Alenia Spazio S.p.A. Naples, Italy)
Waterman, Elly H. (Fokker B.V. Schipol-Oost, Netherlands)
Paillard, Jacques (MATRA Sep Imagerie et Informatique Saint Quentin en Yvelines, France)
Larsen, Peter N. (Reson System A/S Slangerup, Denmark)
Venet, Gerard (METRAVIB Ecully, France)
Goeransson, Peter (Aeronautical Research Inst. of Sweden Bromma., United States)
Martin, Vincent (Centre National de la Recherche Scientifique Marseilles, France)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA. Langley Research Center, Fourth Aircraft Interior Noise Workshop
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 92-2092
Accession Number
92N32956
Funding Number(s)
CONTRACT_GRANT: EEC-AERO-0028-C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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