nasa / TCML
The Tip Clearance Modeling Library (TCML) was developed to model the dynamic variation of the high pressure turbine (HPT) tip clearance in aero-engine turbomachinery. The modeling techniques should be applicable to compressors as well. The model can be driven by prescribed inputs or seamlessly integrated with an aero-engine simulation such as on…
☆16Updated 6 years ago
Alternatives and similar repositories for TCML:
Users that are interested in TCML are comparing it to the libraries listed below
- ☆23Updated 7 years ago
- The Thermal Systems Analysis Toolbox (TSAT) is a MATLAB/Simulink based tool for modeling and analysis of dynamic thermal systems involvin…☆32Updated 6 years ago
- ☆35Updated last year
- Turbomachinery Blade and Flow path design tool☆38Updated this week
- Python module to generate stochastic reduced order models (SROMs)☆43Updated last year
- ☆31Updated 2 months ago
- OpenConcept: A toolkit for conceptual MDAO of aircraft with unconventional propulsion architectures☆40Updated 3 weeks ago
- ☆33Updated last year
- ☆48Updated 6 years ago
- ☆35Updated 2 years ago
- ☆49Updated 4 years ago
- A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.☆19Updated 3 years ago
- Computational Aerodynamics Lab☆23Updated 4 years ago
- conceptual design of vtol platforms☆13Updated 6 years ago
- Gas models, combustion and gas turbine solver.☆70Updated last year
- A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repositor…☆21Updated 7 years ago
- A MATLAB tool for the mean-line design optimization of axial turbines☆31Updated 4 years ago
- An open source, semi-automated, control design tool for subsonic aircraft engine simulations written in the MATLAB/Simulink environment. …☆63Updated 10 years ago
- Centrifugal Pump Design Tool Script☆12Updated last year
- ☆20Updated 7 years ago
- Vortex Lattice for Aeroelasticity☆11Updated 7 years ago
- Aeroelastic Aircraft Design and Simulation Tool☆25Updated 6 years ago
- Uncertainty Quantification using Polynomial Chaos Expansion (UQPCE) is an open source, python based research code for use in parametric, …☆40Updated last month
- ☆67Updated last year
- A pre/post processor for PANAIR☆14Updated 4 years ago
- ☆29Updated 7 years ago
- Matlab code to accompany "Aircraft Aerodynamic Design: Geometry and Optimization" by Sobester and Forrester (2015)☆16Updated 6 years ago
- Blade Element Momentum Theory: developed during my Bachelor Thesis in Aerospace Engineering☆42Updated 2 years ago
- A blade element momentum method for analyzing wind turbine aerodynamic performance that is robust (guaranteed convergence), fast (superli…☆48Updated last year