nasa / Three-Dimensional-Nozzle-Design-Code
☆44Updated 4 years ago
Related projects ⓘ
Alternatives and complementary repositories for Three-Dimensional-Nozzle-Design-Code
- Turbomachinery Blade and Flow path design tool☆31Updated this week
- ☆45Updated 6 years ago
- Non-AXisymmetric aerodynamic design system for turbomachinery☆14Updated 4 years ago
- ☆100Updated last year
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆31Updated 6 years ago
- Computational Aerodynamics Lab☆20Updated 4 years ago
- Python functions for Quasi-1D Gasdynamics☆22Updated this week
- This script plots Bell Nozzle (Thrust Optimised Parabolic (TOP) nozzle) for the given area-ratio and throat radius.☆20Updated 2 months 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…☆42Updated 2 years ago
- ☆30Updated 2 years ago
- A pre/post processor for PANAIR☆14Updated 3 years ago
- MACH: MDO of Aircraft Configurations with High fidelity☆115Updated 3 weeks ago
- PICLas is a parallel, three-dimensional PIC-DSMC solver developed cooperatively by the Institute of Space Systems, Institute of Aerodynam…☆74Updated last month
- Multiphysics with OpenMDAO☆48Updated 2 months ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆27Updated 3 years ago
- Stripped down version of XROTOR as compiled python module☆17Updated last year
- A python based blade parametrization tool☆50Updated 3 months ago
- An Implementation of the Vortex Lattice (VLM) and the Doublet Lattice Method (DLM) for aeroelasticity.☆19Updated 2 months ago
- A Python module for modeling airfoils☆30Updated 11 months ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆18Updated 2 years ago
- Vortex Lattice Method library written in Python☆41Updated 5 years ago
- ☆29Updated 2 months ago
- A python wrapper of the Panair/A502 panel code.☆14Updated 2 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆38Updated 2 years ago
- Finite-element library for analysis and adjoint-based gradient evaluation☆108Updated 2 weeks ago
- Porous Material Analysis Toolbox☆17Updated last year
- Stripped down version of XFOIL as compiled python module☆88Updated 3 years ago
- A Matlab interface for NASA CEA☆30Updated 4 years ago
- Computational Fluid Dynamics, Waves, Reactions, Plasmas☆45Updated 3 weeks ago
- RocketProps calculates the various liquid propellant properties required to analyse a liquid propellant thrust chamber.☆15Updated 5 months ago