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NUMERICAL APPROACH IN AEROELASTICITY

Journal: Scientific Journal of Silesian University of Technology. Series Transport (Vol.93, No. 93)

Publication Date:

Authors : ; ; ; ;

Page : 115-122

Keywords : aeroelasticity; fluid structure interaction; wing;

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Abstract

Aircraft wing design processes should comprise specific analyses oriented towards aeroelasticity, which is one of the essential factors determining flight envelope boundaries. For such cases, static or dynamic aeroelastic phenomena can be simulated using CFD simulation software. ANSYS software offers the fluid structure interaction (FSI) method for solving this multiphysics problem.

Last modified: 2016-12-23 17:14:46