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gas-turbine-cycle

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Expert skill for gas turbine engine thermodynamic cycle analysis and optimization

QUICK START

How to use this skill

Bring this guide into your coding agent with a prompt tailored to the tool you use.

  1. Open your project in Codex.
  2. Copy the prompt below and paste it into your agent.
  3. Review the proposed files and risks before you approve installation.
Prompt to paste
I want to install this Agent Skill for this project in Codex.

Source SKILL.md: https://github.com/a5c-ai/babysitter/blob/HEAD/library/specializations/domains/science/aerospace-engineering/skills/gas-turbine-cycle/SKILL.md

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First, summarize what it does, its dependencies, license status if identifiable, and any risks. Show the exact files you propose to add under .agents/skills/gas-turbine-cycle/. Do not write files or run scripts until I approve.

After I approve, install the complete skill folder, including required referenced files, into that project location. Verify it is discoverable, then tell me its actual invocation name and how to use it. Do not claim it is installed until you have verified it.

Copying this prompt does not install or run the skill. Review third-party files before use. Codex skill guide

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