LEADER 00798nam0-22003011i-450 001 990001746850403321 005 20190529131351.0 035 $a000174685 035 $aFED01000174685 035 $a(Aleph)000174685FED01 035 $a000174685 100 $a20030910d1918----km-y0itay50------ba 101 0 $aita 102 $aIT 200 1 $a<>letteratura ladina nel Friuli$fBindo Chiurlo 210 $aRoma$cL'Universelle$d1918 215 $a42 p.$d23 cm 610 0 $aLetteratura ladina 610 0 $aLingua ladina 676 $a800 700 1$aChiurlo,$bBindo$075716 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aLG 912 $a990001746850403321 952 $a60 OP. 31/37$b38349$fFAGBC 959 $aFAGBC 996 $aLetteratura ladina nel Friuli$9365744 997 $aUNINA LEADER 02006nam 2200481I 450 001 9910703769403321 005 20150603125855.0 035 $a(CKB)5470000002434025 035 $a(OCoLC)910630631 035 $a(EXLCZ)995470000002434025 100 $a20150603j201412 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 13$aAn evaluation of the additional acoustic power needed to overcome the effects of a test-article's absorption during reverberant chamber acoustic testing of spaceflight hardware /$fAron D. Hozman, William O. Hughes 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dDecember 2014. 215 $a1 online resource (8 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2014-218432 300 $aTitle from title screen (viewed on June 3, 2015). 300 $a"December 2014." 300 $a"Prepared for the Noise-Con 2014 sponsored by the Institute of Noise Control Engineering of the USA (INCE/USA), Fort Lauderdale, Florida, September 8-10, 2014." 320 $aIncludes bibliographical references (page 8). 606 $aSound pressure$2nasat 606 $aReverberation chambers$2nasat 606 $aAcoustic simulation$2nasat 606 $aSound generators$2nasat 606 $aAudio equipment$2nasat 615 7$aSound pressure. 615 7$aReverberation chambers. 615 7$aAcoustic simulation. 615 7$aSound generators. 615 7$aAudio equipment. 700 $aHozman$b Aron D.$01411177 702 $aHughes$b William O. 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910703769403321 996 $aAn evaluation of the additional acoustic power needed to overcome the effects of a test-article's absorption during reverberant chamber acoustic testing of spaceflight hardware$93501690 997 $aUNINA