Title of article
Tuned mass dampers for flight vehicle components subjected to rocket noise
Author/Authors
Jain، نويسنده , , P.C. and Mukherjee، نويسنده , , A. and Krishna، نويسنده , , Y.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2011
Pages
8
From page
175
To page
182
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.
Keywords
Rocket noise , Finite elements , Attenuation , Vibrations , tuned mass dampers , Flight vehicles
Journal title
Aerospace Science and Technology
Serial Year
2011
Journal title
Aerospace Science and Technology
Record number
2230393
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