LEADER 01903nam  2200481I  450 
001 9910706215103321
005 20171101140635.0
035   $a(CKB)5470000002456290
035   $a(OCoLC)1008888300
035   $a(EXLCZ)995470000002456290
100   $a20171101j200012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of predicted and measured turbine vane rough surface heat transfer /$fR.J. Boyle, C.M. Spuckler, and B.L. Lucci
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2000.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v2000-210219
300   $a"December 2000."
300   $a"Prepared for the 45th International Gas Turbine and Aeroengine Technical Congress sponsored by the American Society of Mechanical Engineers, Munich, Germany, May 8-11, 2000."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
300   $a"ASME 2000-GT-0217."
320   $aIncludes bibliographical references (pages 14-15).
606   $aHeat transfer$2nasat
606   $aK-omega turbulence model$2nasat
606   $aVanes$2nasat
606   $aSurface roughness$2nasat
615  7$aHeat transfer.
615  7$aK-omega turbulence model.
615  7$aVanes.
615  7$aSurface roughness.
700   $aBoyle$b Robert J.$01387461
702   $aSpuckler$b C. M.
702   $aLucci$b Barbara L.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706215103321
996   $aComparison of predicted and measured turbine vane rough surface heat transfer$93485199
997   $aUNINA