| name | gas-turbine-cycle |
| description | Expert skill for gas turbine engine thermodynamic cycle analysis and optimization |
| allowed-tools | ["Read","Write","Glob","Grep","Edit","WebFetch","WebSearch","Bash"] |
| metadata | {"version":"1.0","category":"aerospace-engineering","tags":["propulsion","gas-turbine","thermodynamics","cycle-analysis"]} |
| graph | {"domains":["domain:aerospace-engineering"],"specializations":["specialization:aerospace-engineering"],"skillAreas":["skill-area:physics-simulation","skill-area:mathematical-reasoning","skill-area:statistical-analysis"],"roles":["role:research-engineer","role:computational-scientist"]} |
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