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Record 47 of 238
Advanced Study for Active Noise Control in Aircraft (ASANCA)
Offline Availability: Go to Request Form
Author and Affiliation:
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)
Abstract: 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.
Publication Date: Jul 01, 1992
Document ID:
19920023712
(Acquired Nov 07, 1995)
Accession Number: 92N32956
Subject Category: ACOUSTICS
Report/Patent Number: AIAA PAPER 92-2092
Document Type: Conference Paper
Publication Information: NASA. Langley Research Center, Fourth Aircraft Interior Noise Workshop; p 129-141
Publisher Information: United States
Contract/Grant/Task Num: EEC-AERO-0028-C
Financial Sponsor: NASA; United States
Organization Source: Dornier Luftfahrt G.m.b.H.; Friedrichshafen, Germany
Description: 13p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: AIRCRAFT COMPARTMENTS; AIRCRAFT NOISE; CRITICAL FREQUENCIES; FLIGHT TESTS; GROUND TESTS; NOISE MEASUREMENT; NOISE PREDICTION (AIRCRAFT); NOISE REDUCTION; VIBRATION MEASUREMENT; COMPUTATIONAL GRIDS; DATA REDUCTION; FINITE ELEMENT METHOD; LOW FREQUENCIES; PERFORMANCE TESTS
Imprint And Other Notes: In NASA. Langley Research Center, Fourth Aircraft Interior Noise Workshop p 129-141 (SEE N92-32948 23-71)
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