#
naca
Here are 9 public repositories matching this topic...
-
Updated
Jul 7, 2023 - OpenSCAD
A set of tools that let you analyze the aerodynamic performance of wings and airfoils using models such as TaT,LLT and VLM.
python
numpy
pyqt5
cfd
aircraft
aerodynamics
wing
airfoil
aerofoil
lifting-line-theory
llt
tat
naca
thin-airfoil-theory
airfoi
high-lift-devices
vortix-lattice-method
-
Updated
Sep 30, 2023 - Python
-
Updated
May 26, 2020 - MATLAB
Vertical wind turbine sandbox simulating the averaged torque on a three-blade vertical turbine with standard NACA blade profiles.
-
Updated
Feb 13, 2022 - Python
Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)
-
Updated
Feb 3, 2021 - MATLAB
Improve this page
Add a description, image, and links to the naca topic page so that developers can more easily learn about it.
Add this topic to your repo
To associate your repository with the naca topic, visit your repo's landing page and select "manage topics."