Paper Info
Title
Isogeometric simulation of turbine blades for aircraft engines
Abstract
Isogeometric analysis is a novel approach to numerical simulation that has the potential to bridge the gap between geometric design and numerical analysis. It uses the same exact geometry representation in all stages of the product development. In this paper we present recent results which demonstrate the competitiveness of the new concept in an industrial environment, more precisely, in the challenging field of aircraft engines. We study the deformation of turbine blades under the assumption of linear elasticity by considering all major loads and boundary conditions of a standard mechanical simulation process for turbine blades. We use the numerical approximations obtained by the classical finite element method as a benchmark for the capabilities of the new concept. It is shown that it is able to reach comparable results using only a small fraction of the number of degrees of freedom required by the classical method. Thus, isogeometric analysis allows using much coarser geometric representations for numerical simulation.
Year
DOI
Venue
2012
10.1016/j.cagd.2012.03.002
Computer Aided Geometric Design
Keywords
Field
DocType
classical finite element method,classical method,numerical analysis,turbine blade,coarser geometric representation,aircraft engine,numerical approximation,isogeometric simulation,isogeometric analysis,standard mechanical simulation process,numerical simulation,new concept,turbine blades
Boundary value problem,Topology,Turbine blade,Computer simulation,Isogeometric analysis,Mechanical engineering,Finite element method,Geometric design,Linear elasticity,Numerical analysis,Mathematics
Journal
Volume
Issue
ISSN
29
7
0167-8396
Citations 
PageRank 
References 
4
0.54
7
Authors
5
Name
Order
Citations
PageRank
David GroíMann140.54
Bert Jüttler2114896.12
Helena Schlusnus340.54
Johannes Barner440.54
Anh-Vu Vuong5444.23