A symmetrical boundary element formulation for sound transmission through fuselage walls -theory, implemetation and test cases-

Thumbnail Image
Files
TP-1996-504.pdf (220.32 KB)
Date
1996
Authors
Grooteman, F.P.
Schippers, H.
Boer, A. de
Journal Title
Journal ISSN
Volume Title
Publisher
National Aerospace Laboratory NLR
Abstract
Description
Keywords
Citation
URI
http://hdl.handle.net/10921/1374
Collections
Reports