On the Dynamic Response Prediction at the Full-Scale Test of Aircraft Component

Abstract

<jats:p>Several general effects of boundary conditions and their adequate description at structural dynamic computational simulation constitute the main subject of the discussion. First, an analytical model of elastically supported beam was considered to evaluate the effects of support compliance to the basic dynamic characteristics. Second, a more complex model of a body with elastic support was simulated. Some general properties of structure dynamics were analysed.

Document type: Article

Original document

The different versions of the original document can be found in:

• https://content.sciendo.com/downloadpdf/journals/tae/4/1/article-p22.pdf under the license https://creativecommons.org/licenses/by-nc-nd

• http://content.sciendo.com/view/journals/tae/4/1/article-p22.xml,

http://www.degruyter.com/view/j/tae.2017.4.issue-1/tae-2017-0003/tae-2017-0003.pdf,

http://dx.doi.org/10.1515/tae-2017-0003 under the license cc-by-nc-nd

• http://www.degruyter.com/view/j/tae.2017.4.issue-1/tae-2017-0003/tae-2017-0003.xml?format=INT,

https://doaj.org/toc/2255-9876 under the license http://creativecommons.org/licenses/by-nc-nd/3.0

• https://content.sciendo.com/view/journals/tae/4/1/article-p22.xml,

https://core.ac.uk/display/87706581,

https://academic.microsoft.com/#/detail/2754223225