LEADER 00819nam0-22003011i-450- 001 990008016510403321 005 20070212125101.0 010 $a0-521-59125-2 035 $a000801651 035 $aFED01000801651 035 $a(Aleph)000801651FED01 035 $a000801651 100 $a20050302d2000----km-y0itay50------ba 101 0 $aeng 105 $ay-------001yy 200 1 $aTurbulent Flows$fStephen B. Pope 210 $aCambridge$cCambridge University Press$d2000 215 $aXXXIV, 771 p.$cill.$d25 cm 700 1$aPope,$bStephen B.$0496951 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008016510403321 952 $a04 161-193$bIRC 1075160$fDINCH 952 $a00 A2547$b5018$fDETEC 959 $aDETEC 959 $aDINCH 996 $aTurbulent flows$943591 997 $aUNINA LEADER 01118cam0-22003731i-450 001 990000422880403321 005 20190506154336.0 035 $a000042288 035 $aFED01000042288 035 $a(Aleph)000042288FED01 035 $a000042288 100 $a20020821d1982----km-y0itay50------ba 101 1 $aita$cger 102 $aIT 105 $aa-------001yy 200 1 $aProgetto ufficio$fO. Gottschalk$gnote a cura di Ferruccio Francescato$grevisione tecnica di Enrico Bertini Malgarini 210 $aMilano$cBE-MA Editrice$d1982 215 $a171 p.$cill.$d30 cm 225 1 $aProgettazione in architettura 454 0$12001$aFlexible Verwaltungsbauten$91551476 700 1$aGottschalk,$bOttomar$0764255 702 1$aBertini Malgarini,$bEnrico 702 1$aFrancescato,$bFernando 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990000422880403321 952 $a08 N 6$fDINED 952 $a223007$b3508$fDCATA 952 $aRGT 1997$b5619$fDARPU 959 $aDARPU 959 $aDINED 959 $aDCATA 996 $aFlexible Verwaltungsbauten$91551476 997 $aUNINA LEADER 01994oam 2200529 450 001 9910713879903321 005 20200825134918.0 035 $a(CKB)5470000002504892 035 $a(OCoLC)1104148324 035 $a(EXLCZ)995470000002504892 100 $a20190610d1956 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAnalysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel /$fby Stanley H. Scher 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1956. 215 $a1 online resource (54 pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3611 300 $a"April 1956." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 22). 606 $aAirplanes$xTesting 606 $aSpin (Aerodynamics) 606 $aWind tunnel testing 606 $aAirplanes$xTesting$2fast 606 $aSpin (Aerodynamics)$2fast 606 $aWind tunnel testing$2fast 615 0$aAirplanes$xTesting. 615 0$aSpin (Aerodynamics) 615 0$aWind tunnel testing. 615 7$aAirplanes$xTesting. 615 7$aSpin (Aerodynamics) 615 7$aWind tunnel testing. 700 $aScher$b Stanley H.$01416899 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bTRAAL 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910713879903321 996 $aAnalysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel$93523777 997 $aUNINA