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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
Ingo U Borchers (Dornier Luftfahrt G.m.b.H. Friedrichshafen, Germany)
Urban Emborg (Saab Aircraft Division)
Antonio Sollo (Alenia Spazio S.p.A. Naples, Italy)
Elly H Waterman (Fokker B.V. Schipol-Oost, Netherlands)
Jacques Paillard (MATRA Sep Imagerie et Informatique Saint Quentin en Yvelines, France)
Peter N Larsen (Reson System A/S Slangerup, Denmark)
Gerard Venet (METRAVIB Ecully, France)
Peter Goransson (The Aeronautical Research Institute of Sweden)
Vincent Martin (Centre National de la Recherche Scientifique Marseilles, France)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: Fourth Aircraft Interior Noise Workshop
Publisher: National Aeronautics and Space Administration
Volume: NASA-CP-10103
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 92-2092
Meeting Information
Meeting: Fourth Aircraft Interior Noise Workshop
Location: Friedrichshafen
Country: DE
Start Date: May 19, 1992
End Date: May 20, 1992
Sponsors: Society of Automotive Engineers International, German Aerospace Center, National Aeronautics and Space Administration
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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