gas-turbine-cycle
Expert skill for gas turbine engine thermodynamic cycle analysis and optimization
Best use case
gas-turbine-cycle is best used when you need a repeatable AI agent workflow instead of a one-off prompt.
Expert skill for gas turbine engine thermodynamic cycle analysis and optimization
Teams using gas-turbine-cycle 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
Manual Installation
- Download SKILL.md from GitHub
- Place it in
.claude/skills/gas-turbine-cycle/SKILL.mdinside your project - Restart your AI agent — it will auto-discover the skill
How gas-turbine-cycle Compares
| Feature / Agent | gas-turbine-cycle | Standard Approach |
|---|---|---|
| Platform Support | Not specified | Limited / Varies |
| Context Awareness | High | Baseline |
| Installation Complexity | Unknown | N/A |
Frequently Asked Questions
What does this skill do?
Expert skill for gas turbine engine thermodynamic cycle analysis and optimization
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
# Gas Turbine Cycle Analysis Skill ## Purpose Provide comprehensive gas turbine engine thermodynamic cycle analysis capabilities for turbofan, turbojet, and turboprop engine design and optimization. ## Capabilities - NPSS and GasTurb model setup and execution - Component matching and off-design analysis - Turbofan, turbojet, turboprop configuration - Performance map generation and interpolation - Bleed and power extraction modeling - Transient performance analysis - SFC optimization studies - Engine inlet and nozzle integration ## Usage Guidelines - Select appropriate component models based on engine configuration - Validate component maps against available test data - Consider off-design performance across the flight envelope - Account for bleed and power extraction in system-level analysis - Optimize cycle parameters for specific mission requirements - Document assumptions and limitations for each analysis ## Dependencies - NPSS (Numerical Propulsion System Simulation) - GasTurb - MATLAB ## Process Integration - AE-004: Gas Turbine Cycle Analysis
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