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Lightweight Ceramics for Aeroacoustic ApplicationsThe use of a HTP (High Temperature Performance) ceramic foam for aeroacoustic applications is investigated. HTP ceramic foam is a composition of silica and alumina fibers developed by LMMS. This foam is a lightweight high-temperature fibrous bulk material with small pore size, ultra high porosity, and good strength. It can be used as a broadband noise absorber at both room and high temperature (up to 1800 F). The investigation included an acoustic assessment as well as material development, and environmental and structural evaluations. The results show that the HTP ceramic foam provides good broadband noise absorbing capability and adequate strength when incorporating the HTP ceramic foam system into a honeycomb sandwich structure. On the other hand, the material is sensitive to Skydrol and requires further improvements. Good progress has been made in the impedance model development. A relationship between HTP foam density, flow resistance, and tortuosity will be established in the near future. Additional effort is needed to investigate the coupling effects between face sheet and HTP foam material.
Document ID
19970027373
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Kwan, H. W.
(Rohr Industries, Inc. Chula Vista, CA United States)
Spamer, G. T.
(Rohr Industries, Inc. Chula Vista, CA United States)
Yu, J.
(Rohr Industries, Inc. Chula Vista, CA United States)
Yasukawa, B.
(Lockheed Martin Missile and Space Sunnyvale, CA United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1997
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:201709
NASA-CR-201709
Report Number: NAS 1.26:201709
Report Number: NASA-CR-201709
Accession Number
97N26351
Funding Number(s)
CONTRACT_GRANT: NAS1-20102
PROJECT: RTOP 538-03-12-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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