Gas Turbine Performance Consulting
  • Home
  • My Services
    • Consultancy
    • Seminars
  • My Tools
    • Compressor Map Fitting
    • Turbine Map Fitting
    • My Performance Software
    • Turbine Map Calculation
  • My Products
    • Compressor Maps
      • NASA Quiet Engine Program Fan B Bypass
      • NASA Quiet Engine Program Fan B Core
      • NASA Energy Efficient Engine Fan Bypass
      • NASA Energy Efficient Engine Fan Core
      • Fan Map Cumpsty
      • Fan Map ASME GT2010-22825
      • 3 Stage Fan NASA CR-2005-213584
      • 3 Stage Subsonic Compressor
      • 6 Stage HPC ISABE 2007-1184
      • 3 Stage Transsonic Compressor - Design Pressure Ratio 4
      • Single Stage Transsonic Compressor - Design Pressure Ratio 1.5
      • Single Stage Radial Compressor - Design Pressure Ratio 5
      • NACA Eight-Stage Compressor
      • 2-Stage Radial Compressor - Design Pressure Ratio 10.5
      • Compressor Map Format
    • Turbine Maps
      • Single Stage Turbine NASA TM 83665
      • 3-Stage Turbine AGARD-LS-195
    • Engine Models
      • BR710
      • F107-WR-400
      • EJ200
      • CFM56-3
      • V2500-A1
      • CFM56-Leap 1A
      • PW1100-JM
      • LM2500
      • LM2500GG
    • Illustrations
    • Tutorials
    • Books
  • More...
    • Activities
    • History
    • My Publications
  • Sitemap

Various illustrations related to gas turbine performance can be found here. Feel free to use them in publications or for teaching purposes.

From here you can download Sankey (Energy) and Grassmann (Exergy) diagrams as well as temperature-entropy diagrams. Engine cross-sections show the exact position of the thermodynamic stations, together with the local temperatures, pressures, velocities, and Mach numbers.

Diagrams drawn to scale are much more useful than cartoons, which only illustrate principles rather than facts. All of the diagrams shown here are to scale.

Send me a GasTurb input file and I will create the corresponding diagrams for your specific data!

All the figures and diagrams  are licensed under Attribution 4.0 International (CC BY 4.0) See: https://creativecommons.org/licenses/by/4.0/legalcode

Read more …

  • Impressum
  • Privacy