LEADER 01397nam--2200409---450- 001 990003404690203316 005 20100526155638.0 010 $a3-8053-2825-7 035 $a000340469 035 $aUSA01000340469 035 $a(ALEPH)000340469USA01 035 $a000340469 100 $a20100526h2002----km-y0itay50------ba 101 $ager 102 $aDE 105 $aaf--||||001yy 200 1 $aGens Augusta$eUntersuchungen zu Aufstellung, Wirkung und Bedeutung der Statuengruppen des julisch-claudischen Kaiserhauses$fDietrich Boschung 210 $aMainz am Rhein$cP. Von Zabern$d2002 215 $aXIV, 233 p., [96] p. di tavole$cill.$e9 carte di tavole ripiegate$d30 cm 225 2 $aMonumenta artis romanae$v32. 410 0$12001$aMonumenta artis romanae$v32. 606 0 $aGiulio-Claudia $xIconografia$2BNCF 606 0 $aScultura romana$zSec. 1. 676 $a733.5 700 1$aBOSCHUNG,$bDietrich$0164908 801 0$aIT$bsalbc$gISBD 912 $a990003404690203316 951 $aXI.5.B. 466$b219200 L.M.$cXI.5.$d00258705 959 $aBK 969 $aUMA 979 $aPAOLA$b90$c20100526$lUSA01$h1032 979 $aPAOLA$b90$c20100526$lUSA01$h1035 979 $aPAOLA$b90$c20100526$lUSA01$h1038 979 $aPAOLA$b90$c20100526$lUSA01$h1039 979 $aPAOLA$b90$c20100526$lUSA01$h1556 996 $aGens Augusta$9280942 997 $aUNISA LEADER 02170nam 2200565I 450 001 9910707310803321 005 20160802155931.0 035 $a(CKB)5470000002464414 035 $a(OCoLC)954498257 035 $a(EXLCZ)995470000002464414 100 $a20160802j199611 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTime-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow /$fKenneth J. Baumeister and Kevin L. Kreider 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dNovember 1996. 215 $a1 online resource (15 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v107363 300 $aTitle from title screen (viewed Aug. 2, 2016). 300 $a"November 1996." 300 $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page 10). 606 $aFinite difference theory$2nasat 606 $aSound propagation$2nasat 606 $aAircraft engines$2nasat 606 $aAeroacoustics$2nasat 606 $aReal time operation$2nasat 606 $aEngine inlets$2nasat 606 $aDucted flow$2nasat 606 $aIterative solution$2nasat 615 7$aFinite difference theory. 615 7$aSound propagation. 615 7$aAircraft engines. 615 7$aAeroacoustics. 615 7$aReal time operation. 615 7$aEngine inlets. 615 7$aDucted flow. 615 7$aIterative solution. 700 $aBaumeister$b Kenneth J.$01400246 702 $aKreider$b Kevin L. 712 02$aLewis Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707310803321 996 $aTime-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow$93532091 997 $aUNINA