USU Aero Lab

Pinned Repositories

AirfoilDatabase
A Python module for modeling airfoils
Language:Python29 6 68
BladeX
Blade Element Propeller Code
Language:FORTRAN13 8 03
MachLine
A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
Language:Fortran26 3 84
MachUp
Numerical Lifting-Line Algorithm
Language:Fortran39 12 315
MachUp_Py
Python Version of MachUp (Numerical Lifting-Line Method)
Language:Python17 12 45
MachUpX
Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
Language:Python86 13 715
panairwrapper
A python wrapper of the Panair/A502 panel code.
Language:Python14 11 15
Pylot
A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.
Language:Python44 8 27
PyPan
A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
Language:Python17 6 03
PyProp
The ultimate electric propulsion modeling and optimization module.
Language:Python15 3 11

USU Aero Lab's Repositories

usuaero/MachUpX
Fast and accurate aerodynamic modeling using general numerical lifting-line theory.
Language:Python86 13 715
usuaero/Pylot
A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.
Language:Python44 8 27
usuaero/MachUp
Numerical Lifting-Line Algorithm
Language:Fortran39 12 315
usuaero/AirfoilDatabase
A Python module for modeling airfoils
Language:Python29 6 68
usuaero/MachLine
A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.
Language:Fortran26 3 84
usuaero/MachUp_Py
Python Version of MachUp (Numerical Lifting-Line Method)
Language:Python17 12 45
usuaero/PyPan
A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.
Language:Python17 6 03
usuaero/PyProp
The ultimate electric propulsion modeling and optimization module.
Language:Python15 3 11
usuaero/panairwrapper
A python wrapper of the Panair/A502 panel code.
Language:Python14 11 15
usuaero/BladeX
Blade Element Propeller Code
Language:FORTRAN13 8 03
usuaero/Optix
Python Gradient-Based Optimization Tool
Language:Python9 9 13
usuaero/Common
Common source files for aero codes
Language:Fortran5 4 02
usuaero/CloudFoil
Language:Fortran4 4 01
usuaero/PropulsionOptimization
Optimize propulsion systems for small UASs
Language:Python3 4 02
usuaero/PyLdB
Calculates the perceived loudness of a pressure signature
Language:Standard ML3 7 04
usuaero/TrajectoryOptimization
A library for optimizing flight trajectories.
Language:Python2 2 01
usuaero/Horizon-Flying-Wing
Base files for the Horizon aircraft for MachUpX and Pylot use.
Language:C1 3 01
usuaero/rapidboom
A tool set for rapid boom prediction of parametric geometries.
Language:Python1 7 01
usuaero/UE5-Flight-Sim
0 2 00
usuaero/fighter_aerodynamics_Nguyen_etal
Aerodynamic data for the fighter aircraft as measured and reported by Nguyen et al. (1979).
Language:Python2 0
usuaero/HI-Mach-Wiki
2 0
usuaero/steady-periodic-lifting-line
Code from the 2021 AeroLab Challenge investigating the steady-periodic lifting line problem.
Language:Python2 0
usuaero/TriPan
A modern, unstructured, subsonic/supersonic flow solver.
Language:Fortran2 01