The influence of lamination angles on the interior noise levels of an aircraft
By: Christian M. Fernholz, Jay H. Robinson.
Contributors: Robinson, Jay H.; Langley Research Center.
Series: NASA technical memorandum -- 110250.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft production.; Cylindrical shells.; Equations of motion.; Finite element method.; Frequency ranges.; Thin walled shells.; Structural design criteria.; Noise reduction.; Noise intensity.; Laminates.
Notes: Shipping list no.: 98-0789-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.