istellartech / OpenLaval
Supersonic Impulse Turbine Blade Design
☆11Updated 6 years ago
Related projects ⓘ
Alternatives and complementary repositories for OpenLaval
- Design of turbomachine blade profile☆26Updated 3 months ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆27Updated 3 years ago
- Turbomachinery Blade and Flow path design tool☆31Updated this week
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆15Updated 5 months ago
- ☆44Updated 4 years ago
- A code based on the Method of Characteristics to solve the supersonic flow inside a nozzle☆11Updated 5 years ago
- Integration of NASA CEA into MATLAB for project at École Polytechnique de Montréal☆11Updated 5 years ago
- T-Blade3 VERSION 1.2: T-Blade3 is a general parametric 3D blade geometry builder. The tool can create a variety of 3D blade geometries ba…☆43Updated 2 years ago
- A Matlab interface for NASA CEA☆30Updated 4 years ago
- Examples for RPA - Tool for Rocket Propulsion Analysis☆16Updated 8 years ago
- OpenFOAM case files for simulating NACA foils.☆43Updated 8 years ago
- A python based blade parametrization tool☆50Updated 3 months ago
- Generate volume meshes for OpenVSP generated surface meshes.☆26Updated 3 years ago
- Python implementation of a client which communicates with the Pointwise Glyph Server.☆24Updated 2 months ago
- Parametrization of the geometry of a turbine blade given the 11 parameters as explained in: L.J. Pritchard: An eleven parameter axial tur…☆19Updated 3 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆58Updated 2 years ago
- ☆17Updated 5 years ago
- Non-AXisymmetric aerodynamic design system for turbomachinery☆14Updated 4 years ago
- Unsteady Vortex Lattice Method for Aeroelasticity in C++☆23Updated last year
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆19Updated 2 months ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆18Updated 2 years ago
- Multall-open is a turbomachinery design system based on the 3D, multistage, Navier-Stokes solver Multall. It can be used to design axial…☆22Updated 5 years ago
- Rocketisp Calculates Delivered Specific Impulse (Isp) For Liquid Rocket Thrust Chambers.☆11Updated 10 months ago
- Generate 4 and 5 digit NACA airfoil sections☆34Updated last month
- Python tool to genreate 2D meshes around airfoils☆24Updated last year
- the open source SU2 mesh format parser and visualizer☆9Updated 4 months ago
- ☆22Updated 12 years ago
- A Python module for modeling airfoils☆30Updated 11 months ago
- Notes and material for ME 461/561 Gas Dynamics course☆22Updated 2 years ago
- Multiphysics with OpenMDAO☆48Updated 2 months ago