nasa / T-MATS
An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) package offers a MATLAB/Simulink toolbox that gives a developer the ability to create simulations of such thermodynamic systems as turbomachinery and gas turbines. Keywords: TMATS, Control System,…
☆251Updated this week
Related projects ⓘ
Alternatives and complementary repositories for T-MATS
- An open source, semi-automated, control design tool for subsonic aircraft engine simulations written in the MATLAB/Simulink environment. …☆57Updated 10 years ago
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆194Updated 3 months ago
- ☆33Updated 10 months ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆36Updated 4 months ago
- Gas models, combustion and gas turbine solver.☆68Updated last year
- A Matlab interface for NASA CEA☆30Updated 4 years ago
- CEASIOMpy is a Python conceptual aircraft design environment☆77Updated this week
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆127Updated this week
- ☆459Updated 6 months ago
- NASA's aircraft analysis, design, and optimization tool☆140Updated last week
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆53Updated last week
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆71Updated 6 months ago
- Turbomachinery Blade and Flow path design tool☆31Updated this week
- CPACS - Common Parametric Aircraft Configuration Schema☆81Updated 3 weeks ago
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆264Updated this week
- A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repositor…☆19Updated 6 years ago
- Some usefull routines for aeroelastic analysis with NASTRAN.☆18Updated 2 years ago
- Calculation of gas turbine cycle☆16Updated 6 years ago
- FAST-(OAD)-GA is a framework for performing rapid Overall Aircraft Design for General Aviation Aircraft☆30Updated last month
- A python library for generating PDF XDSM diagrams.☆59Updated 11 months ago
- ☆30Updated last month
- Multiphysics with OpenMDAO☆48Updated 2 months ago
- An Aircraft Design Toolbox☆415Updated 8 months ago
- Blade Element Momentum Method for Propellers and Turbines☆58Updated last month
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆38Updated 2 years ago
- Proposals for OpenMDAO Enhancements☆14Updated 3 months ago
- Hypersonic / Rarefied gas dynamics code developments (GPL-3.0)☆226Updated last year
- ☆283Updated 2 years ago
- Resources for analyzing aircraft structures for aerospace engineers☆35Updated 4 years ago
- NASTRAN is the NASA Structural Analysis System, a finite element analysis program (FEA)☆143Updated 8 years ago