nasa / T-MATSLinks
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,…
☆297Updated 11 months ago
Alternatives and similar repositories for T-MATS
Users that are interested in T-MATS are comparing it to the libraries listed below
Sorting:
- An open source, semi-automated, control design tool for subsonic aircraft engine simulations written in the MATLAB/Simulink environment. …☆67Updated 11 years ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆53Updated last month
- ☆36Updated last year
- CEASIOMpy is a Python conceptual aircraft design environment☆134Updated this week
- OpenAeroStruct is a lightweight tool that performs aerostructural optimization using OpenMDAO.☆239Updated 2 months ago
- Gas models, combustion and gas turbine solver.☆77Updated 2 years ago
- Simulation of High Aspect Ratio aeroplanes and wind turbines in Python: a nonlinear aeroelastic code☆170Updated 3 weeks ago
- An Aircraft Design Toolbox☆488Updated last year
- NASA's aircraft analysis, design, and optimization tool☆241Updated last week
- A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repositor…☆22Updated 8 years ago
- FAST-OAD: An open source framework for rapid Overall Aircraft Design☆76Updated 3 weeks ago
- The Tip Clearance Modeling Library (TCML) was developed to model the dynamic variation of the high pressure turbine (HPT) tip clearance i…☆21Updated 7 years ago
- Turbomachinery Blade and Flow path design tool☆68Updated this week
- An interactional aerodynamics and acoustics solver for multirotor aircraft and wind energy☆336Updated 3 months ago
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆37Updated 7 years ago
- ☆324Updated 3 years ago
- Tucan remains among the simplest and most user friendly programs for aerodynamics based on vortex lattice methods. This project is unique…☆79Updated last year
- A Matlab interface for NASA CEA☆34Updated 6 years ago
- CPACS - Common Parametric Aircraft Configuration Schema☆97Updated 2 months ago
- Thermodynamic cycle modeling library, built on top of OpenMDAO☆144Updated 2 months ago
- ☆40Updated 2 years ago
- Python interface for XFOIL. The objective of this library is to be able to be able to call XFOIL from Python iteratively for any simulati…☆76Updated 4 years ago
- RocketCEA Wraps The NASA Fortran CEA Code☆125Updated 8 months ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆55Updated 3 years ago
- Wind Plant Integrated System Design and Engineering Model☆170Updated last week
- Multiphysics with OpenMDAO☆113Updated last week
- Aeroelastic Aircraft Design and Simulation Tool☆29Updated 7 years ago
- A python library for generating PDF XDSM diagrams.☆71Updated 3 months ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆37Updated 4 years ago
- Implementation of the Blade Element Momentum Theory for turbines and propellers in Python☆80Updated 3 years ago