NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Quiet Honeycomb PanelsSandwich honeycomb composite panels are lightweight and strong, and, therefore, provide a reasonable alternative to the aluminum ring frame/stringer architecture currently used for most aircraft airframes. The drawback to honeycomb panels is that they radiate noise into the aircraft cabin veil- efficiently provoking the need for additional sound treatment which adds weight and reduces the material's cost advantage. A series of honeycomb panels was made -hick incorporated different design strategies aimed at reducing the honeycomb panels' radiation efficiency while at the same time maintaining their strength. The majority of the designs were centered around the concept of creating areas of reduced stiffness in the panel by adding voids and recesses to the core. The effort culminated with a reinforced/recessed panel which had 6 dB higher transmission loss than the baseline solid core panel while maintaining comparable strength.
Document ID
20100017150
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Palumbo, Daniel L.
(NASA Langley Research Center Hampton, VA, United States)
Klos, Jacob
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2010
Subject Category
Composite Materials
Report/Patent Number
NF1676L-9856
Report Number: NF1676L-9856
Meeting Information
Meeting: Joint 159th Meeting of the Acoustical Society of America and Noise-Con 2010
Location: Baltimore, MD
Country: United States
Start Date: April 19, 2010
End Date: April 23, 2010
Funding Number(s)
WBS: WBS 561581.02.08.07.18.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available