LEADER 01852nam  2200517   450 
001 9910707155303321
005 20170630094040.0
035   $a(CKB)5470000002461945
035   $a(OCoLC)992440009
035   $a(EXLCZ)995470000002461945
100   $a20170630j198510    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 II /$fby W.H. Atkinson, M.A. Cyr, R.R. Strange
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, NASA Lewis Research Center,$dOctober 1985.
215   $a1 online resource (viii, 77 pages) $cillustration
225 1 $aNASA CR ;$v174995
300   $a"October 1985."
300   $a"Performing organization: United Technologies Corporation, Pratt & Whitney, Engineering Division"--Report documentation page.
300   $a"PWA-5914-39."
320   $aIncludes bibliographical references (pages 75-77).
517 3 $aTurbine blade and vane heat flux sensor development phase 2
606   $aCross flow$2nasat
606   $aHeat flux$2nasat
606   $aHeat transfer$2nasat
606   $aHeat transfer coefficients$2nasat
606   $aTurbine blades$2nasat
615  7$aCross flow.
615  7$aHeat flux.
615  7$aHeat transfer.
615  7$aHeat transfer coefficients.
615  7$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   $a9910707155303321
996   $aTurbine blade and vane heat flux sensor development phase II$93436430
997   $aUNINA