LEADER 00872nam0-22003011i-450- 001 990004615600403321 005 20050120154143.0 035 $a000461560 035 $aFED01000461560 035 $a(Aleph)000461560FED01 035 $a000461560 100 $a19990604d1982----km-y0itay50------ba 101 0 $aita 105 $ay-------001yy 200 1 $a<>STORIA locale$etemi, fonti e metodi della ricerca$fa cura di Cinzio Violante 210 $aBologna$cIl Mulino$dc1982. 215 $a193 p.$d22 cm 610 0 $aStoriografia italiana. 676 $a907.2045$v21$zita 702 1$aViolante,$bCinzio$f<1921-2001> 801 0$aIT$bUNINA$gRICA$2UNIMARC 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990004615600403321 952 $a907.20 VIO 1$bI.st.r.c.3309$fFLFBC 959 $aFLFBC 996 $aSTORIA locale$9551575 997 $aUNINA LEADER 01788oam 2200493 450 001 9910716021303321 005 20210528125959.0 035 $a(CKB)5470000002517895 035 $a(OCoLC)1150919730 035 $a(EXLCZ)995470000002517895 100 $a20200416d1936 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 12$aA method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y /$fby H.A. Pearson 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1936. 215 $a1 online resource (19 pages, 12 unnumbered pages) $cillustrations 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 571 300 $a"June 1936." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 18). 606 $aAerofoils 606 $aSplit flaps (Airplanes) 606 $aAerodynamics$xForecasting 606 $aAerofoils$2fast 606 $aSplit flaps (Airplanes)$2fast 615 0$aAerofoils. 615 0$aSplit flaps (Airplanes) 615 0$aAerodynamics$xForecasting. 615 7$aAerofoils. 615 7$aSplit flaps (Airplanes) 700 $aPearson$b Henry A$g(Henry Adolph),$f1906-$01398867 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910716021303321 996 $aA method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y$93463074 997 $aUNINA