LEADER 01900nam  2200493I  450 
001 9910706550803321
005 20171201081119.0
035   $a(CKB)5470000002456939
035   $a(OCoLC)1013716219
035   $a(EXLCZ)995470000002456939
100   $a20171201j200105    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCoarse grid modeling of turbine film cooling flows using volumetric source terms /$fJames D. Heidmann, Scott D. Hunter
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dMay 2001.
215   $a1 online resource (9 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210817
300   $a"May 2001."
300   $a"Prepared for the 2001 Turbo Expo sponsored by the American Society of Mechanical Engineers, New Orleans, Louisiana, June 4-7, 2001."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
300   $a"2001-GT-138."
320   $aIncludes bibliographical references (page 9).
606   $aComputer aided design$2nasat
606   $aFilm cooling$2nasat
606   $aFlow distribution$2nasat
606   $aMultiblock grids$2nasat
606   $aVolumetric analysis$2nasat
615  7$aComputer aided design.
615  7$aFilm cooling.
615  7$aFlow distribution.
615  7$aMultiblock grids.
615  7$aVolumetric analysis.
700   $aHeidmann$b James D.$01407008
702   $aHunter$b Scott D.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706550803321
996   $aCoarse grid modeling of turbine film cooling flows using volumetric source terms$93510604
997   $aUNINA