USU Aero Lab

MachUpX

Fast and accurate aerodynamic modeling using general numerical lifting-line theory.

Pylot

A fully-featured flight simulator, capable of real-time lifting-line aerodynamic modelling.

MachUp

Numerical Lifting-Line Algorithm

MachLine

A modern, subsonic-supersonic, unstructured, aerodynamic panel code. We do linear aerodynamics for the twenty-first century.

AirfoilDatabase

A Python module for modeling airfoils

MachUp_Py

Python Version of MachUp (Numerical Lifting-Line Method)

PyPan

A panel-based flow solver. Currently in beta but with working solvers for incompressible and inviscid hypersonic flow.

PyProp

The ultimate electric propulsion modeling and optimization module.

panairwrapper

A python wrapper of the Panair/A502 panel code.

BladeX

Blade Element Propeller Code

Optix

Python Gradient-Based Optimization Tool

Common

Common source files for aero codes

CloudFoil

PyLdB

Calculates the perceived loudness of a pressure signature

PropulsionOptimization

Optimize propulsion systems for small UASs

TrajectoryOptimization

A library for optimizing flight trajectories.

Horizon-Flying-Wing

Base files for the Horizon aircraft for MachUpX and Pylot use.

rapidboom

A tool set for rapid boom prediction of parametric geometries.

UE5-Flight-Sim

aircraft_geometry

This repository is designed to assist the creation of MachupX input files given user measurements.

fighter_aerodynamics_Nguyen_etal

Aerodynamic data for the fighter aircraft as measured and reported by Nguyen et al. (1979).

HI-Mach-Wiki

steady-periodic-lifting-line

Code from the 2021 AeroLab Challenge investigating the steady-periodic lifting line problem.

TriPan

A modern, unstructured, subsonic/supersonic flow solver.