02281oam 2200625 a 450 991070206340332120121102113718.0(CKB)5470000002423493(OCoLC)815767578(EXLCZ)99547000000242349320121102d1998 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines[electronic resource] /A.A. Ameri, E. Steinthorsson, David L. Rigby[Cleveland, Ohio] :National Aeronautics and Space Administration, Lewis Research Center,[1998]1 online resource (12 pages) illustrationsNASA/CR ;1998-208514Title from title screen (viewed on Nov. 2, 2012)."August 1998.""Prepared for the Turbo Expo '98 sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998.""ICOMP-98-04."Includes bibliographical references (page 12).Gas turbinesnasatHeat transfernasatAxial flow turbinesnasatBlade tipsnasatClearancesnasatRecessesnasatGas-turbinesHeatTransmissionSchool recess breaksGas turbines.Heat transfer.Axial flow turbines.Blade tips.Clearances.Recesses.Gas-turbines.HeatTransmission.School recess breaks.Ameri Ali A1384587Steinthorsson Erlendur1414358Rigby D. L(David Lester),1963-1414359Lewis Research Center.ASME Turbo Expo(1998 :Stockholm, Sweden)GPOGPOGPOBOOK9910702063403321Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines3513399UNINA