TY - CHAP A1 - Schörner, Roman A1 - Bestle, Dieter T1 - Coupled Optimization of Compressor Blade Roots and Rotor Grooves for Industrial Gas-Turbines T2 - 5th IC-SCCE International Conference: From Scientific Computing to Computational Engineering N2 - Substituting an intuitive human design search by an automated design process for compressor blade roots and rotor grooves driven by numerical optimization. The design of industrial gas turbines is a highly complex task where the engineer typically run a lot of design cases intuitively and manually in order to find only acceptable design solution which is usually a time consuming procedure. Research project funded by Alstom, Switzerland. The research shows the benefit of applying optimization methods to an industrial design process. KW - optimization, FE analysis, compressor blade root, rotor groove, gas turbine Y1 - 2012 UR - http://www.epsmso.gr/all_conf_index/index.html SN - 978-960-98941-9-7 ER -