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dc.contributor.authorJain, P.
dc.contributor.authorMukherjee, Abhijit
dc.contributor.authorKrishna, Y.
dc.date.accessioned2017-01-30T12:07:29Z
dc.date.available2017-01-30T12:07:29Z
dc.date.created2016-09-12T08:36:42Z
dc.date.issued2011
dc.identifier.citationJain, P. and Mukherjee, A. and Krishna, Y. 2011. Tuned mass dampers for flight vehicle components subjected to rocket noise. Aerospace Science and Technology. 15 (3): pp. 175-182.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/18360
dc.identifier.doi10.1016/j.ast.2010.11.004
dc.description.abstract

In this study, response of a flight vehicle component to rocket noise is considered. Tuned mass dampers, hitherto used in low frequency excitation, have been utilized to attenuate high frequency, broad band excitations. Modally tuned dampers have been investigated for a variety of input excitations. Modal dampers exhibit significant attenuation of all input signals. © 2010 Elsevier Masson SAS.

dc.publisherElsevier Masson
dc.titleTuned mass dampers for flight vehicle components subjected to rocket noise
dc.typeJournal Article
dcterms.source.volume15
dcterms.source.number3
dcterms.source.startPage175
dcterms.source.endPage182
dcterms.source.issn1270-9638
dcterms.source.titleAerospace Science and Technology
curtin.departmentOffice of Research and Development
curtin.accessStatusFulltext not available


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