STRESS AND MODAL ANALISYS REPORT FOR AVERT PROGRAM
Journal Title: INCAS BULLETIN - Year 2009, Vol 1, Issue 1
Abstract
This report presents a modal and a static analysis of the assembly wing-flap ,using the finite element software’s ANSYS 11 PATRAN-NASTRAN 2007. The geometry was created in Catia V5 R18and imported. The results from the modal analysis refer to the natural frequencies and represent the displacement vector sum for each frequency. For the static analysis, 17 zones of pressure were chosen. For each zone the pressures values were calculated using the pressure distribution resulted from the INCAS subsonic wind tunnel experiments. For this analysis the results consist in the displacement vector sum and the Von Mises equivalent stress.
Authors and Affiliations
Bogdan CALOIAN, Dorin LOZICI, Radu BISCA
Keywords
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- EP ID EP113597
- DOI 10.13111/2066-8201.2009.1.1.6
- Views 74
- Downloads 0
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