Numerische Optimierung dreidimensional parametrisierter ...

[44] Krammer, P.; Baier, R.-D.; Kurzke, J.; Teuber, M.: Initiatives in Design Methodology forModern Aero-Engines.ISABE 99-7177, 1999.[45] LaMarsh, W. J.; Walsh, J. L.; Rogers, J. L.: Aerodynamic Performance Optimization of aRotor Blade Using a Neural Network as the Analysis.AIAA 92-4837, 1992.[46] Langston, L. S.: Secondary Flows in Axial Turbines - a Review.Heat Transfer in Gas Turbine Systems, Vol. 934, Annals of the New York Academy ofSciences, 2001.[47] Madavan, N. K.; Rai, M., M.; Huber, F.: Neural Net-Based Redesign of a Gas GeneratorTurbine for Improved Unsteady Aerodynamic Performance.AIAA 99-2522, 1999.[48] Mayle, R. E.: The Role of Laminar-Turbulent Transition in Gas Turbine Engines.ASME 91-GT-261, 1991.[49] Meauzé, G.: Overview on Blading Design Methods.AGARD Lecture Series "Blading Design for Axial Turbomachines", No. 167, 1989.[50] Mitchell, M.: An Introduction to Gentic Algorithms.MIT Press, 1998.[51] Montgomery, D. C.: Design and Analysis of Experiments.John Wiley and Sons, 5th edition, 2001.[52] Nagel, M. G.: Untersuchungen am Turbinengitter T106Dopt zur Bestimmung der Profildruckverteilungenin vier Schnitten, der Seitenwanddruckverteilung und des Strömungsfeldeshinter dem Gitter, sowie der Gittercharakteristik bei Variation von Ma 2th undRe 2th .Institutsbericht, LRT-WE12-2002/08, 2002.[53] Nodé-Langlois, T.: Sensitivity Analysis for the Aerodynamic and Dynamical Optimizationof Turbomachinery Airfoils.Diplomarbeit, Projet de fin d’études, MTU Aero Engines München, 2000.[54] Orlowski, M.; Tang., W.: A System for Aerodynamic Optimization of Three-DimensionalConfigurations.NATO-RTO Panel Meeting Ottawa, 1999.114