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:
Online Access:https://purl.fdlp.gov/GPO/gpo30483

MARC

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245 1 0 |a Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines /  |c Daniel E. Paxson, Thomas A. Kaemming. 
264 1 |a Cleveland, Ohio :  |b National Aeronautics and Space Administration, Glenn Research Center,  |c [2012] 
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500 |a Title from title screen (viewed on Oct. 25, 2012). 
500 |a "Prepared for the 50th Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics Nashville, Tennessee, January 9-12, 2012." 
500 |a "May 2012." 
504 |a Includes bibliographical references (page 12). 
500 |a "AIAA-2012-770." 
536 |a Sponsored by National Aeronautics and Space Administration  |h WBS 031102.02.03.0832.11 
536 |d E-18174 
500 |a Electronic resource. 
650 7 |a Gas turbines.  |2 nasat 
650 7 |a Combustion chambers.  |2 nasat 
650 7 |a Flow distribution.  |2 nasat 
650 7 |a Pressure ratio.  |2 nasat 
650 7 |a Thermodynamics.  |2 nasat 
650 7 |a Extraction.  |2 nasat 
650 7 |a Detonation.  |2 nasat 
650 7 |a Combustion.  |2 nasat 
700 1 |a Kaemming, Thomas A. 
711 2 |a AIAA Aerospace Sciences Meeting  |n (50th :  |d 2012 :  |c Nashville, Tenn.) 
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