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High intensity acoustic tests of a thermally stressed aluminum plate in TAFAAn investigation was conducted in the Thermal Acoustic Fatigue Apparatus at the Langley Research Center to study the acoustically excited random motion of an aluminum plate which is buckled due to thermal stresses. The thermal buckling displacements were measured and compared with theory. The general trends of the changes in resonances frequencies and random responses of the plate agree with previous theoretical prediction and experimental results for a mechanically buckled plate.
Document ID
19890011407
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ng, Chung Fai
(NASA Langley Research Center Hampton, VA, United States)
Clevenson, Sherman A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Subject Category
Acoustics
Report/Patent Number
NAS 1.15:101552
NASA-TM-101552
Report Number: NAS 1.15:101552
Report Number: NASA-TM-101552
Accession Number
89N20778
Funding Number(s)
PROJECT: RTOP 506-80-31-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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