The influence of lamination angles on the interior noise levels of an aircraft /

Bibliographic Details
Main Authors:	Fernholz, Christian M. (Christian Michael) (Author), Robinson, J. H. (Jay Howard), 1960- (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 1996.
Series:	NASA technical memorandum ; 110250.
Subjects:	Aircraft production. Cylindrical shells. Equations of motion. Finite element method. Frequency ranges. Thin walled shells. Structural design criteria. Noise reduction. Noise intensity. Laminates.
Online Access:	https://purl.fdlp.gov/GPO/gpo67749

Description
Item Description:	Title from title screen (viewed June 21, 2016). "August 1996." "Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
Physical Description:	1 online resource (vi, 83 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 36-39).