01921nam 2200505I 450 991070491090332120140908093724.0(CKB)5470000002446640(OCoLC)890130997(EXLCZ)99547000000244664020140908j201301 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierThe influence of unsteadiness on the analysis of pressure gain combustion devices /Daniel E. Paxson, Tom KaemmingCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,January 2013.1 online resource (16 pages) color illustrationsNASA/TM ;2013-217831Title from title screen (viewed July 9, 2014)."January 2013.""Prepared for the 51st Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics, Grapevine, Texas, January 7-10, 2013.""AIAA-2013-0280."Includes bibliographical references (page 16).Thermodynamic efficiencynasatCombustionnasatPerformance predictionnasatThermodynamic cyclesnasatSteady flownasatThermodynamic efficiency.Combustion.Performance prediction.Thermodynamic cycles.Steady flow.Paxson Daniel E.1386438Kaemming TomNASA Glenn Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910704910903321The influence of unsteadiness on the analysis of pressure gain combustion devices3439579UNINA