LEADER 00828nam0-22002891i-450- 001 990008122440403321 005 20050531165935.0 035 $a000812244 035 $aFED01000812244 035 $a(Aleph)000812244FED01 035 $a000812244 100 $a20050531d1983----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $a--------001yy 200 1 $aGuida rapida fiscale$eper tutte le categorie dei contribuenti...$fRaffaele Rizzardi 210 $aRoma$cBuffetti e Pirola editori$d1983 215 $aIV, 253 p.$d24 cm 610 0 $aFisco$aLegislazione fiscale 700 1$aRizzardi,$bRaffaele$089391 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008122440403321 952 $aGEN B 207$b13574$fFARBC 959 $aFARBC 996 $aGuida rapida fiscale$9758627 997 $aUNINA LEADER 01938oam 2200517I 450 001 9910707007803321 005 20160406123325.0 035 $a(CKB)5470000002461414 035 $a(OCoLC)703662848 035 $a(EXLCZ)995470000002461414 100 $a20110224j199704 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aInlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack /$fKevin R. Walsh [and three others] 210 1$aEdwards, California.:$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$dApril 1997. 215 $a1 online resource (45 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v104329 300 $aTitle from title screen (viewed April 6, 2016). 300 $a"April 1997." 300 $a"Performing organization: Analytical Services & Materials, Inc. [and] General Electric Aircraft Engines"--Report documentation page. 320 $aIncludes bibliographical references (pages 26-27). 606 $aF-18 aircraft$2nasat 606 $aAngle of attack$2nasat 606 $aAerodynamic characteristics$2nasat 606 $aPressure recovery$2nasat 606 $aEngine inlets$2nasat 615 7$aF-18 aircraft. 615 7$aAngle of attack. 615 7$aAerodynamic characteristics. 615 7$aPressure recovery. 615 7$aEngine inlets. 700 $aWalsh$b Kevin R.$0223814 712 02$aAnalytical Services & Materials, Inc. 712 02$aGE Aircraft Engines (Firm) 712 02$aNASA Dryden Flight Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bSSN 801 1$bSSN 801 2$bGPO 906 $aBOOK 912 $a9910707007803321 996 $aInlet distortion for an F$93547666 997 $aUNINA