Gas Turbine Cycle Analysis Skill
SkillDev toolsExpert skill for gas turbine engine thermodynamic cycle analysis and optimization
Instructions available. Your AI can read the instructions. Execution depends on the setup they require.
Account requirements not reviewed. Check the skill instructions before use; ahel provides instructions and does not run this skill.
Add ahel to your AI once: Claude, ChatGPT, Cursor, Claude Code or Codex. Then ask it to use this.
Then ask your AI: use the Gas Turbine Cycle Analysis Skill skill
What this skill tells your AI
The instructions your AI receives, as published by a5c-ai/babysitter in library/specializations/domains/science/aerospace-engineering/skills/gas-turbine-cycle/SKILL.md and read by ahel’s review.
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
Signals
- GitHub stars
- 2k
- Forks
- 112
- Last commit
- Sep 2026
Advanced
- Item type
- skill
- Key
gas-turbine-cycle- Source
- github.com/a5c-ai/babysitter