02045nam 2200493I 450 991070364020332120150416110046.0(CKB)5470000002433310(OCoLC)907472897(EXLCZ)99547000000243331020150416j201403 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierUpdates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements /Changju Thomas Wey and Nan-Suey LiuCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,March 2014.1 online resource (14 pages) color illustrationsNASA/TM ;2014-218108Title from title screen (viewed on April 16, 2015)."March 2014.""Prepared for the SciTech 2014 sponsored by the American Institute of Aeronautics and Astronautics, National Harbor, Maryland, January 13-17, 2014."Includes bibliographical references (page 14).Computational fluid dynamicsnasatNavier-Stokes equationnasatGrid generation (mathematics)nasatLarge eddy simulationnasatGrid refinement (mathematics)nasatComputational fluid dynamics.Navier-Stokes equation.Grid generation (mathematics)Large eddy simulation.Grid refinement (mathematics)Wey Changju Thomas1398080Liu Nan-SueyNASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910703640203321Updates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements3460708UNINA