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The Institute of Theoretical and Applied Mechanics
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Original version of the author's contribution as presented on CD, section: CD-MS 03 PROGRESS AND CHALLENGES IN SPACECRAFT STRUCTURAL DYNAMICS .:
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An Easy-To-Implement Computational Method for the Spacecraft Sine Test-Prediction With Particular Emphasis on the Modal Contributions
Nali, P.
;
Caccamo, L.
A methodology useful for calculating the frequency response functions in terms of interface forces and local accelerations of a hard-mounted structure subjected to base-s [...]
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