Flow Matching Results of an Mhd Energy Bypass System on a Supersonic Turbojet Engine Using the Numerical Propulsion System Simulation (Npss) Environme

by National Aeronautics and Space Administration

Flow matching has been successfully achieved for an MHD energy bypass system on a supersonic turbojet engine. The Numerical Propulsion System Simulation (NPSS) environment helped perform a thermodynamic cycle analysis to properly match the flows from an inlet employing a MHD energy bypass system (consisting of an MHD generator and MHD accelerator) on a supersonic turbojet engine. Working with various operating conditions (such as the applied magnetic...

• Format: Paperback
• Language: English
• ISBN: 1794337873
• ISBN13: 9781794337879
• Release Date: January 1
• Publisher: Independently Published
• Length: 26 Pages
• Weight: 0.19 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"