USU Aero Lab (usuaero)

USU Aero Lab

usuaero

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Home Page:http://aero.go.usu.edu

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USU Aero Lab's repositories

MachUpX

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

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Pylot

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

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MachUp

Numerical Lifting-Line Algorithm

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AirfoilDatabase

A Python module for modeling airfoils

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MachLine

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

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MachUp_Py

Python Version of MachUp (Numerical Lifting-Line Method)

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PyPan

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

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PyProp

The ultimate electric propulsion modeling and optimization module.

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panairwrapper

A python wrapper of the Panair/A502 panel code.

BladeX

Blade Element Propeller Code

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Optix

Python Gradient-Based Optimization Tool

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Common

Common source files for aero codes

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PropulsionOptimization

Optimize propulsion systems for small UASs

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PyLdB

Calculates the perceived loudness of a pressure signature

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TrajectoryOptimization

A library for optimizing flight trajectories.

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Horizon-Flying-Wing

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

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rapidboom

A tool set for rapid boom prediction of parametric geometries.

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fighter_aerodynamics_Nguyen_etal

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

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steady-periodic-lifting-line

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

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TriPan

A modern, unstructured, subsonic/supersonic flow solver.

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