LEADER 01276nam0-2200421---450 001 990009911500403321 005 20170721121214.0 010 $a978-88-08-18694-2 035 $a000991150 035 $aFED01000991150 035 $a(Aleph)000991150FED01 100 $a20141029d2014----km-y0itaa50------ba 101 0 $aita 102 $aIT 105 $aa---a---001yy 200 1 $aDalle funzioni ai modelli$eil calcolo per le bioscienze$fDario Benedetto, Mirko Degli Esposti, Carlotta Maffei 210 $aMilano$cCea$dİ2014 215 $aviii, 307 p.$cill. (col.)$d27 cm 610 0 $aCalcolo 610 0 $aScienze della vita$aMatematica 676 $a570.151$v22$zita 676 $a515$v21$zita 700 1$aBenedetto,$bDario$0315961 701 1$aDegli Esposti,$bMirko$067821 701 1$aMaffei,$bCarlotta$0432433 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990009911500403321 952 $a570.151-BEN-1$b8125$fSC1 952 $a570.151-BEN-1A$b8126$fSC1 952 $a570.151-BEN-1B$b8127$fSC1 952 $a570.151-BEN-1C$b8128$fSC1 952 $a570.151-BEN-1D$b8129$fSC1 952 $aD-74-BDM-001$bingr. 19/2017$fMA1 959 $aSC1 959 $aMA1 996 $aDalle funzioni ai modelli$9831833 997 $aUNINA LEADER 02524oam 2200685I 450 001 9910709611203321 005 20180613083158.0 035 $a(CKB)5470000002472128 035 $a(OCoLC)761342529 035 $a(EXLCZ)995470000002472128 100 $a20111115j198504 ua 0 101 0 $aeng 135 $aurun||||a|a|| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEffects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane /$fDonald L. Hughes, Lawrence P. Myers, and Karen G. Mackall 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$d1985. 215 $a1 online resource (20 pages) $cillustrations 225 1 $aNASA/TP ;$v2411 300 $a"April 1985." 300 $aPrepared at the Dryden Flight Research Facility. 320 $aIncludes bibliographical references (page 6). 606 $aStatic pressure$2nasat 606 $aAircraft engines$2nasat 606 $aInlet flow$2nasat 606 $aFlight tests$2nasat 606 $aPressure measurement$2nasat 606 $aStatic pressure probes$xTesting 606 $aAirplanes$xTurbojet engines$xAir intakes 606 $aEagle (Jet fighter plane) 606 $aAirplanes$xTurbojet engines$xAir intakes$2fast 606 $aEagle (Jet fighter plane)$2fast 615 7$aStatic pressure. 615 7$aAircraft engines. 615 7$aInlet flow. 615 7$aFlight tests. 615 7$aPressure measurement. 615 0$aStatic pressure probes$xTesting. 615 0$aAirplanes$xTurbojet engines$xAir intakes. 615 0$aEagle (Jet fighter plane) 615 7$aAirplanes$xTurbojet engines$xAir intakes. 615 7$aEagle (Jet fighter plane) 700 $aHughes$b Donald L$g(Donald Lee),$f1926-$01410119 702 $aMyers$b Lawrence P. 702 $aMackall$b Karen G. 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch, 712 02$aAmes Research Center. 712 02$aHugh L. Dryden Flight Research Center. 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCO 801 2$bOCLCQ 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910709611203321 996 $aEffects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane$93498168 997 $aUNINA