• Home
  • About GSP
  • Licensing
  • Support
  • Services
  • Downloads
  • Contact
  • Login
  • Disclaimer
Main Menu
  • Home
  • About GSP
  • Licensing
  • Support
  • Services
  • Downloads
    • Case Studies
      • Variable speed Micro Gas Turbine for cogeneration application
      • Lift-fan driven by afterburning turbofan
      • Generation of TT4/TT2 lines in the compressor map
      • Low calorific gasification products as alternative fuel for an industrial gas turbine engine
      • Turbofan performance at specified engine thrust
    • Documentation
    • GSP 11
    • Sample Models
nlrlogo.png

Case Studies

Share your experience!

We encourage users to send in their case studies, showing creative use of GSP. If you think your study is interesting to publish on our website, please contact us through the contact form.

Remember to not include any proprietary information. Before actual publishing you will of course be asked for final acceptance.

The author of every published case study will be awarded a free GSP Standard license (only valid for non-profit users)!

 

Case studies
The following studies are available and displayed in print-friendly format:

Generation of TT4/TT2 lines in the compressor map

This case study by Mark Oostveen shows how to generate lines for constant TT4/TT2 in the compressor map and how to obtain a first scheme for an engine control system.

Variable speed Micro Gas Turbine

This case study by Antonino Pontecorvo shows creative use of the standard GSP LE components to find the operating domain of a micro gas turbine running on various (biomass) fuels.

Turbofan performance at specified engine thrust

This TUD/NLR case study shows the use of the Thrust Control component available in the Supplementary Component Library.

Lift-fan driven by afterburning turbofan

This NLR case study shows the use of the STOVL components available in the GSP STOVL Component Library.

Low calorific gasification products as alternative fuel for an industrial gas turbine engine

This TUD/NLR case study shows the use of a low calorific fuel instead of liquified natural gas and propses solutions to problems that arise due to the increased mass flow.
 

Copyright National Aerospace Laboratory NLR 2010
All Rights Reserved.