LEADER 00786nam0-22002771i-450- 001 990000999210403321 005 20101108103814.0 035 $a000099921 035 $aFED01000099921 035 $a(Aleph)000099921FED01 035 $a000099921 100 $a20001205d1960----km-y0itay50------ba 101 0 $aeng 200 1 $aElements of physical chemistry$fSamuel Glasstone and David Lewis 210 $aPrinceton [N.J.]$cVan Nostrand$d1960 610 0 $aChimica fisica 676 $a541 700 1$aGlasstone,$bSamuel$f<1897-1986>$0923 701 1$aLewis,$bDavid$032348 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990000999210403321 952 $a36B-003.003$b1686$fFI1 959 $aFI1 996 $aElements of physical chemistry$9354282 997 $aUNINA LEADER 02209oam 2200601I 450 001 9910713762603321 005 20200729141810.0 035 $a(CKB)5470000002504057 035 $a(OCoLC)1100474463 035 $a(EXLCZ)995470000002504057 100 $a20190508d1949 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10? to 9.0 x 10? /$fby Laurence K. Loftin, Jr. and Hamilton A. Smith 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1949. 215 $a1 online resource (75 pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1945 300 $a"October 1949." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 17). 517 3 $aAerodynamic characteristics of fifteen National Advisory Committee for Aeronautics airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6) 606 $aAerofoils 606 $aAerodynamics 606 $aReynolds number 606 $aAerodynamics$2fast 606 $aAerofoils$2fast 606 $aReynolds number$2fast 606 $aAerodynamic characteristics$2nasat 606 $aAirfoil profiles$2nasat 615 0$aAerofoils. 615 0$aAerodynamics. 615 0$aReynolds number. 615 7$aAerodynamics. 615 7$aAerofoils. 615 7$aReynolds number. 615 7$aAerodynamic characteristics. 615 7$aAirfoil profiles. 700 $aLoftin$b Laurence K.$01398356 702 $aSmith$b Hamilton A. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bCOP 801 2$bTRAAL 801 2$bGPO 906 $aBOOK 912 $a9910713762603321 996 $aAerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10? to 9.0 x 10?$93462005 997 $aUNINA