Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype /

Bibliographic Details

Corporate Authors:	NASA Glenn Research Center, AIAA Aerospace Sciences Meeting
Other Authors:	DeLaat, John C.
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217617.
Subjects:	Combustion stability. Gas turbine engines. Pressure sensors. Combustion chambers. Dynamic pressure. Adaptive control. Combustion control.
Online Access:	https://purl.fdlp.gov/GPO/gpo31847