Compressor Maps

Hello GasTurb, GSP, pyCycle, T-MATS, PROOSIS and NPSS users!  You need compressor maps for your performance studies? I can generate them for you! 

The source of your map may be a figure from a publication, calculated or measured data as text file, and input data from your favourite performance program. Extending the map down to 1% spool speed and to pressure ratios less than unity - as needed for starting and windmilling simulations - is not a problem.

Here are maps that have been extended down to 1% of the design spool speed both in GasTurb and NPSS format:

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

Single Stage Transsonic Compressor - Design Pressure Ratio 1.5

Single Stage Fan - Design Pressure Ratio 1.7

Single Stage Fan - Design Pressure Ratio 2.47

3 Stage Fan - Design  Pressure Ratio 3.44

3 Stage Subsonic Compressor - Design Pressure Ratio 2.25

3-Stage Transsonic Compressor - Design Pressure Ratio 4

6-Stage HPC - Design Pressure Ratio 8

8-Stage Comressor Without VGV's - Design Pressure Ratio 10

Single Stage Radial Compressor - Design Pressure Ratio 5

2-Stage Radial Compressor - Design Pressure Ratio 10

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

GasTurb is a trademark of GasTurb GmbH, Aachen, Germany