turbomachinery

Imperial College London Aeronautical Engineering (MEng 4YFT) Study Materials

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

A Python Turbomachinery design library for liquid rocket engine applications.

Open toolkit for high fidelity simulation of turbomachinery aerodynamics based on the 3DNS solver

Non-AXisymmetric aerodynamic design system for turbomachinery

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)

Automated mesher for turbomachinery applications

Automated mesher for turbomachinery applications

Performance analysis of turbojet and turbofan engines.

Tutorials of the open-source CFD solver code_saturne, created by Simvia

GPPS CFD Workshop data

Thermodynamic modelling of a gas turbine Brayton cycle using MATLAB to compare constant and temperature-dependent specific heat effects on efficiency and performance.

Parametric centrifugal compressor impeller geometry generation using PyTurbo for turbomachinery design and aerodynamic workflow development.

An LLM agent that drives OpenFOAM end-to-end — meshing, MRF rotating machinery, conjugate heat transfer — with a self-evolving tool framework validated against published experiments

This repository has computation of centrifugal pump (Mesh Convergence and Validation Study Done) evaluating the head and efficiency vs mass flow rate and noted the working rage of centrifugal pump.

Compute the resultant force and pressure center (center of pressure) of any pressure-loaded surface — turbomachinery blades, aircraft wings, car spoilers, building walls, hulls, etc. — from surface pressure point clouds. Python + NumPy/SciPy.

Reduced steady RANS/CHT benchmark of NASA C3X Run 145 using Ansys Fluent 26.1 and Python.