Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1718743 | Aerospace Science and Technology | 2011 | 8 Pages |
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.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
P.C. Jain, A. Mukherjee, Y. Krishna,