Two-dimensional blade-to-blade and three-dimensional simulations are performed with the CFD toolbox OpenFOAM. For two-dimensional through-flow computations a compressible streamline curvature method was implemented. One-dimensional preliminary analysis is done with Calc and an extended mean line program, where loss models are already included. The geometry of turbomachine blades is described with a newly developed NURBS based blade designer. Some relevant software already existed and few additional components were required, which have been developed mainly by students and are available at .tum.de. This paper demonstrates an aerodynamic design process for turbomachines for compressible flows, using exclusively open source software tools. Journal of Verification, Validation and Uncertainty Quantification.Journal of Thermal Science and Engineering Applications.Journal of Offshore Mechanics and Arctic Engineering.Journal of Nuclear Engineering and Radiation Science.Journal of Nondestructive Evaluation, Diagnostics and Prognostics of Engineering Systems.Journal of Nanotechnology in Engineering and Medicine.Journal of Micro and Nano-Manufacturing.Journal of Manufacturing Science and Engineering.Journal of Engineering Materials and Technology.Journal of Engineering for Sustainable Buildings and Cities.Journal of Engineering for Gas Turbines and Power.
Journal of Engineering and Science in Medical Diagnostics and Therapy.Journal of Electrochemical Energy Conversion and Storage.Journal of Dynamic Systems, Measurement, and Control.Journal of Computing and Information Science in Engineering.Journal of Computational and Nonlinear Dynamics.Journal of Autonomous Vehicles and Systems.ASME Letters in Dynamic Systems and Control.ASCE-ASME Journal of Risk and Uncertainty in Engineering Systems, Part B: Mechanical Engineering.Mechanical Engineering Magazine Select Articles.
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