Aircraft interior acoustic noise control
Name
44085265-MIT.pdf
Description
Full printable version
Size
1.87 MB
Format
Adobe PDF
Checksum (MD5)
314b2fe0a2ef21b4f807526ff51d39b3
Author(s)
Copley-Woods, Djuna S. (Djuna Sunlight), 1977-
Advisor(s)
Mauro J. Atalla and Michael L. Fripp.
Date Issued
1999
Publisher
Massachusetts Institute of Technology
Abstract
An experimental study was perfonned to determine which materials are best suited for internal aircraft noise reduction. An impedance tube with dimensions of a scaled aircraft was constructed and evaluated, and eleven materials were tested and compared based on their noise reduction properties, weight, and thickness. Polyvinylidene Fluoride was tested for use in active noise control for a large space.
Description
Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1999.
Includes bibliographical references (p. 45).
Subjects
Mechanical Engineering.
MIT Department
Massachusetts Institute of Technology. Department of Mechanical Engineering
Terms of Use
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