LEADER 01881nam  2200529   450 
001 9910705729803321
005 20170630084523.0
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035   $a(OCoLC)992437789
035   $a(EXLCZ)995470000002453111
100   $a20170630j198408    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTurbine blade and vane heat flux sensor development phase 1 /$fby W.H. Atkinson, M.A. Cyr, R.R. Strange
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dAugust, 1984.
215   $a1 online resource (viii, 87 pages, 2 unnumbered pages) $cillustration
225 1 $aNASA-CR ;$v168297
300   $a"August, 1984."
300   $a"Performing organization: United Technologies Corporation, Pratt & Whitney, Engineering Division"--Report documentation page.
300   $a"PWA-5914-21."
320   $aIncludes bibliographical references (pages 60-64).
606   $aGas turbine engines$2nasat
606   $aHeat flux$2nasat
606   $aHeat resistant alloys$2nasat
606   $aThermal cycling tests$2nasat
606   $aThermocouples$2nasat
606   $aTurbine blades$2nasat
615  7$aGas turbine engines.
615  7$aHeat flux.
615  7$aHeat resistant alloys.
615  7$aThermal cycling tests.
615  7$aThermocouples.
615  7$aTurbine blades.
700   $aAtkinson$b W. H.$01387010
702   $aCyr$b M. A.
702   $aStrange$b R. R.
712 02$aLewis Research Center,
712 02$aPratt & Whitney Aircraft Group.$bEngineering Division.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705729803321
996   $aTurbine blade and vane heat flux sensor development phase 1$93512736
997   $aUNINA