TY - CHAP A1 - Sommer, Lars A1 - Bestle, Dieter T1 - Speeding-up 2D Aerofoil Design by Using Curvature Constraints Y1 - 2008 ER - TY - CHAP A1 - Flassig, Peter Michael A1 - Dutta, Amit Kumar A1 - Bestle, Dieter T1 - Robustheit und Zuverlässigkeit in der aerodynamischen Verdichterauslegung Y1 - 2008 ER - TY - CHAP A1 - Bestle, Dieter A1 - Keskin, Akin A1 - Otto, Dierk T1 - Process Integration and Automation for optimal Design Y1 - 2006 ER - TY - CHAP A1 - Dutta, Amit Kumar A1 - Flassig, Peter Michael A1 - Otto, Dierk A1 - Bestle, Dieter T1 - Process Integration for Multidisciplinary Multi-objective Blade Design Y1 - 2007 ER - TY - CHAP A1 - Hinz, Michel A1 - Bestle, Dieter T1 - Implementation of Individual iSIGHT-FD Components for Process Acceleration by Wrapping of FORTRAN-Routines Y1 - 2009 ER - TY - GEN A1 - Bestle, Dieter A1 - Hinz, Michel A1 - Rühle, Tobias T1 - Unterstützende Strategien für den robusten Triebwerksentwurf - Durch Prozessintegration, problemspezifische Parametrisierung und Mehrkriterien-Optimierung zum Erfolg KW - Mehrkriterien-Optimierung Y1 - 2009 ER - TY - CHAP A1 - Flassig, Peter Michael A1 - Bestle, Dieter T1 - Probabilistische Studien zur robusten aerodynamischen Verdichterauslegung Y1 - 2009 ER - TY - CHAP A1 - Rogge, Stephan A1 - Amtsfeld, Philipp A1 - Hentschel, Christian A1 - Bestle, Dieter A1 - Meyer, Marcus T1 - Using gestures to interactively modify turbine blades in a Virtual Environment T2 - Emerging Signal Processing Applications (ESPA), 2012 IEEE International Conference, Las Vegas, 12 - 14 Jan. 2012 KW - GPU-accelerated computational fluid dynamics KW - blade geometry;cumbersome input hardware KW - expensive input hardware KW - fluid flow KW - gesture-based interaction KW - interactively modify turbine blades KW - special interaction;virtual environments KW - blades;computational fluid dynamics KW - gesture recognition KW - graphics processing units KW - turbines Y1 - 2012 SN - 978-1-4673-0899-1 SP - 155 EP - 158 PB - IEEE ER - 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 - TY - GEN A1 - Kahlbau, Sebastian A1 - Bestle, Dieter T1 - Optimal Shift Control for Automatic Transmission T2 - Mechanics Based Design of Structures and Machines Y1 - 2013 SN - 1539-7742 VL - 41 IS - 3 SP - 259 EP - 273 ER -