01800nam 2200469I 450 991070581080332120170811105536.0(CKB)5470000002454313(OCoLC)1000386845(EXLCZ)99547000000245431320170811j201707 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAxial-flow turbine rotor discharge-flow overexpansion and limit-loading conditionpart 1Computational fluid dynamics (CFD) investigation /Shu-Cheng S. ChenCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,July 2017.1 online resource (iii, 37 pages)NASA/TM ;2017-219506"July 2017."Includes bibliographical references (page 37).pt. 1. Computational fluid dynamics (CFD) investigation.Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition. part 1, Computational fluid dynamics Computational fluid dynamicsnasatAxial flow turbinesnasatTurbine blades. formulanasatSupercritical flownasatCritical flownasatComputational fluid dynamics.Axial flow turbines.Turbine blades. formula.Supercritical flow.Critical flow.Chen Shu-Cheng S.1410451NASA Glenn Research Center,GPOGPOBOOK9910705810803321Axial-flow turbine rotor discharge-flow overexpansion and limit-loading condition3516729UNINA