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gas-turbine-cycle

gas-turbine-cycle

Expert skill for gas turbine engine thermodynamic cycle analysis and optimization

Independent GitHub snapshot · Automated classification · Original documentation governs

Documentation de la Skill

GitHub

name: gas-turbine-cycle description: Expert skill for gas turbine engine thermodynamic cycle analysis and optimization allowed-tools:

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  • 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
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