02167nam 2200577Ia 450 991070212210332120121026085137.0(CKB)5470000002424920(OCoLC)814446445(EXLCZ)99547000000242492020121026d2012 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierFoundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines[electronic resource] /Daniel E. Paxson, Thomas A. KaemmingCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (12 pages) color illustrationsNASA/TM ;2012-217443Title 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 (page 12).Gas turbinesnasatCombustion chambersnasatFlow distributionnasatPressure rationasatThermodynamicsnasatExtractionnasatDetonationnasatCombustionnasatGas turbines.Combustion chambers.Flow distribution.Pressure ratio.Thermodynamics.Extraction.Detonation.Combustion.Paxson Daniel E1386438Kaemming Thomas A1418636NASA Glenn Research Center.AIAA Aerospace Sciences Meeting(50th :2012 :Nashville, Tenn.)GPOGPOBOOK9910702122103321Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines3530621UNINA