SciBlend: Advanced Data Visualization Workflows within Blender.
Pythonic spectral proper orthogonal decomposition
A MATLAB tool for the mean-line design optimization of axial turbines
Parametrization of the geometry of a turbine blade given the 11 parameters as explained in: L.J. Pritchard: An eleven parameter axial turbine airfoil geometry model
Non-AXisymmetric aerodynamic design system for turbomachinery
Open toolkit for high fidelity simulation of turbomachinery aerodynamics based on the 3DNS solver
Automated mesher for turbomachinery applications
A Python Turbomachinery design library for liquid rocket engine applications.
The VINK compressor is an open-access compressor geometry designed as part of a collaboration project with partners from Swedish univerities and industry (Chalmers University of Technology, KTH Royal Institute of Technology, Lund University, GKN Aerospace Sweden AB, and Swerea)
Performance analysis of turbojet and turbofan engines.
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