01020nam--2200373---450-99000337598020331620100303161220.084-7307-027-5000337598USA01000337598(ALEPH)000337598USA0100033759820100303d1973----km-y0itay50------baspaES||||||||001yyUsuras y figuracionespoesía 1952-1972Carlos BarralLas Palmas de Gran CanariaInventarios provisionales1973206 p.20 cmLetras a su imán2001Letras a su imán2001001-------2001Poesia spagnola861.6BARRAL,Carlos164656ITsalbcISBD990003375980203316II.5.A.552113 DSLLBKDSLLDSLL9020100303USA011612Usuras y figuraciones1123061UNISA01800nam 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