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100   $a20130912j200007    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAugmentation of stagnation region heat transfer due to turbulence from a DLN can combustor /$fG. James Van Fossen, Ronald S. Bunker
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJuly 2000.
215   $a1 online resource (9 pages) $cillustrations
225 1 $aNASA/TM ;$v2000-210219
300   $a"July 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-0215."
320   $aIncludes bibliographical references (pages 8-9).
517 3 $aAugmentation of stagnation region heat transfer due to turbulence from a Dry-Low-NOx can combustor
606   $aAugmentation$2nasat
606   $aStagnation point$2nasat
606   $aFlow distribution$2nasat
606   $aHeat transfer$2nasat
606   $aGas turbines$2nasat
606   $aTurbulent flow$2nasat
606   $aIsotropic turbulence$2nasat
615  7$aAugmentation.
615  7$aStagnation point.
615  7$aFlow distribution.
615  7$aHeat transfer.
615  7$aGas turbines.
615  7$aTurbulent flow.
615  7$aIsotropic turbulence.
700   $aVanFossen$b G. James$01394113
702   $aBunker$b Ronald S.
712 02$aNASA Glenn Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706214703321
996   $aAugmentation of stagnation region heat transfer due to turbulence from a DLN can combustor$93450984
997   $aUNINA