LEADER 02710oam 2200769I 450 001 9910713763603321 005 20200729120056.0 035 $a(CKB)5470000002504047 035 $a(OCoLC)1100474419 035 $a(EXLCZ)995470000002504047 100 $a20190508d1948 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections /$fby Laurence K. Loftin, Jr. and Kenneth S. Cohen 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1948. 215 $a1 online resource (37 pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1591 300 $aTitle from title screen (viewed March 7, 2019). 300 $a"June 1948." 300 $a"Langley Memorial Aeronautical Laboratory, Langley Field, Va." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 14). 517 3 $aAerodynamic characteristics of a number of modified National Advisory Committee for Aeronautics four-digit-series airfoil sections 606 $aAerofoils 606 $aAerodynamics 606 $aFlaps (Airplanes) 606 $aAerodynamic load 606 $aLift (Aerodynamics) 606 $aDrag (Aerodynamics) 606 $aPitching (Aerodynamics) 606 $aAerodynamic load$2fast 606 $aAerodynamics$2fast 606 $aAerofoils$2fast 606 $aDrag (Aerodynamics)$2fast 606 $aFlaps (Airplanes)$2fast 606 $aLift (Aerodynamics)$2fast 606 $aPitching (Aerodynamics)$2fast 615 0$aAerofoils. 615 0$aAerodynamics. 615 0$aFlaps (Airplanes) 615 0$aAerodynamic load. 615 0$aLift (Aerodynamics) 615 0$aDrag (Aerodynamics) 615 0$aPitching (Aerodynamics) 615 7$aAerodynamic load. 615 7$aAerodynamics. 615 7$aAerofoils. 615 7$aDrag (Aerodynamics) 615 7$aFlaps (Airplanes) 615 7$aLift (Aerodynamics) 615 7$aPitching (Aerodynamics) 700 $aLoftin$b Laurence K.$01398356 702 $aCohen$b Kenneth S. 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 $a9910713763603321 996 $aAerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections$93503328 997 $aUNINA