Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines /

Bibliographic Details

Main Author:	Paxson, Daniel E.
Corporate Authors:	AIAA Aerospace Sciences Meeting, NASA Glenn Research Center
Other Authors:	Kaemming, Thomas A.
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217443.
Subjects:	Gas turbines. Combustion chambers. Flow distribution. Pressure ratio. Thermodynamics. Extraction. Detonation. Combustion.
Online Access:	https://purl.fdlp.gov/GPO/gpo30483