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Finite Element Development and Specifications of a Patched, Recessed Nomex Core Honeycomb Panel for Increased Sound Transmission LossThis informal report summarizes the development and the design specifications of a recessed nomex core honeycomb panel in fulfillment of the deliverable in Task Order 13RBE, Revision 10, Subtask 17. The honeycomb panel, with 0.020-inch thick aluminum face sheets, has 0.016-inch thick aluminum patches applied to twenty-five, 6 by 6 inch, quarter inch thick recessed cores. A 10 dB higher transmission loss over the frequency range 250 - 1000 Hz was predicted by a MSC/NASTRAN finite element model when compared with the transmission loss of the base nomex core honeycomb panel. The static displacement, due to a unit force applied at either the core or recessed core area, was of the same order of magnitude as the static displacement of the base honeycomb panel when exposed to the same unit force. The mass of the new honeycomb design is 5.1% more than the base honeycomb panel. A physical model was constructed and is being tested.
Document ID
20070031764
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Grosveld, Ferdinand W.
(Lockheed Martin Engineering and Science Services Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
September 1, 2007
Subject Category
Acoustics
Report/Patent Number
NASA/CR-2007-214898
Report Number: NASA/CR-2007-214898
Funding Number(s)
CONTRACT_GRANT: NAS1-00135B
WBS: WBS 561581.02.08.07.18.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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