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

Transport and Aerospace Engineering 2017
Vitālijs Pavelko, Aleksandrs Ņevskis

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.

Keywords
Aircraft component, computational simulation, dynamics test, strength
DOI
10.1515/tae-2017-0003

Pavelko, V., Ņevskis, A. On the Dynamic Response Prediction at the Full-Scale Test of Aircraft Component. Transport and Aerospace Engineering, 2017, 4, pp.22-28. ISSN 2255-968X. e-ISSN 2255-9876. Available from: doi:10.1515/tae-2017-0003

Publication language
English (en)