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

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

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Bibliographic Details
Author / Creator:Paxson, Daniel E.
Imprint:Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Description:1 online resource (12 p.) : col. ill.
Language:English
Series:NASA/TM ; 2012-217443
NASA technical memorandum ; 2012-217443.
Subject:
Combustion.
Combustion chambers.
Gas-turbines.
Thermodynamics.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8941064
Hidden Bibliographic Details
Other authors / contributors:Kaemming, Thomas A.
NASA Glenn Research Center.
AIAA Aerospace Sciences Meeting (50th : 2012 : Nashville, Tenn.)
Notes:Title from title screen (viewed on Oct. 25, 2012).
"Prepared for the 50th Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics Nashville, Tennessee, January 9-12, 2012."
"May 2012."
"AIAA-2012-770."
Includes bibliographical references (p. 12).
Sponsored by National Aeronautics and Space Administration WBS 031102.02.03.0832.11
E-18174
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2012-217443

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