hypersonic-aerothermo

Specialized skill for hypersonic vehicle aerodynamic and thermal analysis

509 stars

Best use case

hypersonic-aerothermo is best used when you need a repeatable AI agent workflow instead of a one-off prompt.

Specialized skill for hypersonic vehicle aerodynamic and thermal analysis

Teams using hypersonic-aerothermo should expect a more consistent output, faster repeated execution, less prompt rewriting.

When to use this skill

  • You want a reusable workflow that can be run more than once with consistent structure.

When not to use this skill

  • You only need a quick one-off answer and do not need a reusable workflow.
  • You cannot install or maintain the underlying files, dependencies, or repository context.

Installation

Claude Code / Cursor / Codex

$curl -o ~/.claude/skills/hypersonic-aerothermo/SKILL.md --create-dirs "https://raw.githubusercontent.com/a5c-ai/babysitter/main/library/specializations/domains/science/aerospace-engineering/skills/hypersonic-aerothermo/SKILL.md"

Manual Installation

  1. Download SKILL.md from GitHub
  2. Place it in .claude/skills/hypersonic-aerothermo/SKILL.md inside your project
  3. Restart your AI agent — it will auto-discover the skill

How hypersonic-aerothermo Compares

Feature / Agenthypersonic-aerothermoStandard Approach
Platform SupportNot specifiedLimited / Varies
Context Awareness High Baseline
Installation ComplexityUnknownN/A

Frequently Asked Questions

What does this skill do?

Specialized skill for hypersonic vehicle aerodynamic and thermal analysis

Where can I find the source code?

You can find the source code on GitHub using the link provided at the top of the page.

SKILL.md Source

# Hypersonic Aerothermodynamics Skill

## Purpose
Provide specialized hypersonic vehicle aerodynamic and thermal analysis capabilities including real gas effects, aerodynamic heating, and thermal protection system design.

## Capabilities
- High-temperature gas dynamics
- Real gas effects modeling
- Aerodynamic heating prediction
- Thermal protection system sizing
- Shock-boundary layer interaction
- Ablation modeling
- Transition prediction (hypersonic)
- Chemically reacting flow analysis

## Usage Guidelines
- Account for real gas and chemical non-equilibrium effects
- Use appropriate turbulence models for hypersonic boundary layers
- Predict transition location and heating augmentation
- Size TPS with adequate margins for heating uncertainty
- Consider ablation effects on aerodynamic shape
- Validate predictions against ground test data where available

## Dependencies
- High-fidelity CFD codes
- Real-gas models
- Thermal protection system design tools

## Process Integration
- AE-001: CFD Analysis Workflow (hypersonic regime)
- Advanced hypersonic vehicle design processes