LEADER 01187nam0-22003731i-450- 001 990007890000403321 005 20060628165532.0 020 $aIT 035 $a000789000 035 $aFED01000789000 035 $a(Aleph)000789000FED01 035 $a000789000 100 $a20040526d2000----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $ay-------001yy 200 1 $aLezioni di progettazione degli impianti industriali$fMarco Garetti (a cura di)$gAnna Bartolotta, Sergio Cavalieri, Marco Taisch$gredazione a cura di Elena Corradi 205 $a3. ed 210 $aMilano$cCUSL$dstampa 2000 215 $a125 p.$cill$d24 cm 300 $aIn testa al front.: Diploma universitario di Ingegneria logistica e della produzione 610 0 $aImpianti$aProgettazione 676 $a658.2$v20$zita 702 1$aTaisch,$bMarco 702 1$aGaretti,$bMarco 702 1$aCavalieri,$bSergio 702 1$aBartolotta,$bAnna 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990007890000403321 952 $aTECN B 1506$b12756$fFARBC 959 $aFARBC 996 $aLezioni di progettazione degli impianti industriali$9668196 997 $aUNINA LEADER 02282oam 2200589 450 001 9910706214703321 005 20171101145812.0 035 $a(CKB)5470000002456294 035 $a(OCoLC)858249949 035 $a(EXLCZ)995470000002456294 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