| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 291897 | Journal of Sound and Vibration | 2006 | 5 Pages |
Abstract
The dynamic response of a thermal data capture unit is calculated for a given missile flight test environment. Power spectral densities calculated from the analytical model were compared with the experimental results. Maximum peak displacements were used to calculate clearances required during the installation phase of system assembly.
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Authors
N. Bhutani,