flow-inviscid 0.2.0

Inviscid supersonic and hypersonic surface solutions: Taylor-Maccoll, Newtonian, tangent-cone, shock-expansion

flow-inviscid

Computes inviscid surface Mach number, pressure, and temperature along a body contour using classical methods such as tangent-cone, tangent-wedge, Modified Newtonian, shock-expansion, method of characteristics, and linearized supersonic.

Install

pip install flow-inviscid

Quick Start

under construction

Documentation

Full documentation: https://uahypersonics.github.io/flow-inviscid

Validation and Verification

under construction

Code Style

This project follows established Python community conventions so that contributors can focus on the physics rather than inventing formatting rules.

Convention	What it covers	Reference
PEP 8	Code formatting, naming, whitespace	Python standard style guide
PEP 257	Docstring structure	Python standard docstring conventions
numpydoc	Docstring sections (Parameters, Returns, Attributes)	NumPy/SciPy docstring standard
Ruff	Automated linting and formatting	Enforces PEP 8 compliance automatically

Releasing

This project uses Semantic Versioning (vMAJOR.MINOR.PATCH):

• MAJOR (v1.0.0): Breaking API changes
• MINOR (v0.3.0): New features, backward-compatible
• PATCH (v0.3.1): Bug fixes

To publish a new version:

1. Verify locally:

   ruff check .
   pytest
   

2. Commit and push to main
3. Tag and push:

   git tag -a vMAJOR.MINOR.PATCH -m "Release vMAJOR.MINOR.PATCH"
   git push origin vMAJOR.MINOR.PATCH
   

Citation