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