%0 Journal Article
%T AEROTAXI ground static test and finite element model validation
%A Dorin LOZICI-BRINZEI
%A Simion TATARU
%A Radu BISCA
%J INCAS Bulletin
%D 2011
%I National Institute for Aerospace Research ˇ°Elie Carafoliˇ± - INCAS
%R 10.13111/2066-8201.2011.3.2.6
%X In this presentation, we will concentrate on typical Ground Static Test (GST) and Finite Element (FE) software comparisons. It is necessary to note, that standard GST are obligatory for any new aircraft configuration. We can mention here the investigations of the AeroTAXITM, a small aircraft configuration, using PRODERA  equipment. A Finite Element Model (FEM) of the AeroTAXITM has been developed in PATRAN/NASTRAN , partly from a previous ANSYS  model. FEM can be used to investigate potential structural modifications or changes with realistic component corrections. Model validation should be part of every modern engineering analysis and quality assurance procedure.
%K finite element analysis
%K ground static test
%K strain gauge
%U http://bulletin.incas.ro/files/lozici_dorin_v3_is2_ful.pdf