An Adaptive Instability Suppression Controls Method for Aircraft Gas Turbine Engine Combustors

By: Nasa, National Aeronautics and Space Adm

An adaptive controls method for instability suppression in gas turbine engine combustors has been developed and successfully tested with a realistic aircraft engine combustor rig. This testing was part of a program that demonstrated, for the first time, successful active combustor instability control in an aircraft gas turbine engine-like environment. The controls method is called Adaptive Sliding Phasor Averaged Control. Testing of the control method...

• Format: Paperback
• Language: English
• ISBN: 1793903980
• ISBN13: 9781793903983
• Release Date: January 1
• Publisher: Independently Published
• Length: 26 Pages
• Weight: 0.19 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"