02282oam 2200589 450 991070621470332120171101145812.0(CKB)5470000002456294(OCoLC)858249949(EXLCZ)99547000000245629420130912j200007 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierAugmentation of stagnation region heat transfer due to turbulence from a DLN can combustor /G. James Van Fossen, Ronald S. BunkerCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,July 2000.1 online resource (9 pages) illustrationsNASA/TM ;2000-210219"July 2000.""Prepared for the 45th International Gas Turbine and Aeroengine Technical Congress sponsored by the American Society of Mechanical Engineers, Munich, Germany, May 8-11, 2000.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page."ASME 2000-GT-0215."Includes bibliographical references (pages 8-9).Augmentation of stagnation region heat transfer due to turbulence from a Dry-Low-NOx can combustorAugmentationnasatStagnation pointnasatFlow distributionnasatHeat transfernasatGas turbinesnasatTurbulent flownasatIsotropic turbulencenasatAugmentation.Stagnation point.Flow distribution.Heat transfer.Gas turbines.Turbulent flow.Isotropic turbulence.VanFossen G. James1394113Bunker Ronald S.NASA Glenn Research Center,OCLCEOCLCEOCLCOOCLCQGPOBOOK9910706214703321Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor3450984UNINA