01881nam 2200529 450 991070572980332120170630084523.0(CKB)5470000002453111(OCoLC)992437789(EXLCZ)99547000000245311120170630j198408 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierTurbine blade and vane heat flux sensor development phase 1 /by W.H. Atkinson, M.A. Cyr, R.R. StrangeCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,August, 1984.1 online resource (viii, 87 pages, 2 unnumbered pages) illustrationNASA-CR ;168297"August, 1984.""Performing organization: United Technologies Corporation, Pratt & Whitney, Engineering Division"--Report documentation page."PWA-5914-21."Includes bibliographical references (pages 60-64).Gas turbine enginesnasatHeat fluxnasatHeat resistant alloysnasatThermal cycling testsnasatThermocouplesnasatTurbine bladesnasatGas turbine engines.Heat flux.Heat resistant alloys.Thermal cycling tests.Thermocouples.Turbine blades.Atkinson W. H.1387010Cyr M. A.Strange R. R.Lewis Research Center,Pratt & Whitney Aircraft Group.Engineering Division.GPOGPOBOOK9910705729803321Turbine blade and vane heat flux sensor development phase 13512736UNINA