LEADER 02531oam 2200697I 450 001 9910713762303321 005 20200729144450.0 035 $a(CKB)5470000002504060 035 $a(OCoLC)1100474481 035 $a(EXLCZ)995470000002504060 100 $a20190508d1949 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10? to 11.0 x 10? /$fby Raymond F. Schaefer and Hamilton A. Smith 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1949. 215 $a1 online resource (12 pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1998 300 $a"December 1949." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 8). 517 3 $aAerodynamic characteristics of the National Advisory Committee for Aeronautics 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6) 606 $aAerofoils 606 $aAerodynamics 606 $aLift (Aerodynamics) 606 $aDrag (Aerodynamics) 606 $aPitching (Aerodynamics) 606 $aWind tunnel testing 606 $aAerodynamics$2fast 606 $aAerofoils$2fast 606 $aDrag (Aerodynamics)$2fast 606 $aLift (Aerodynamics)$2fast 606 $aPitching (Aerodynamics)$2fast 606 $aWind tunnel testing$2fast 615 0$aAerofoils. 615 0$aAerodynamics. 615 0$aLift (Aerodynamics) 615 0$aDrag (Aerodynamics) 615 0$aPitching (Aerodynamics) 615 0$aWind tunnel testing. 615 7$aAerodynamics. 615 7$aAerofoils. 615 7$aDrag (Aerodynamics) 615 7$aLift (Aerodynamics) 615 7$aPitching (Aerodynamics) 615 7$aWind tunnel testing. 700 $aSchaefer$b Raymond F.$01410898 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 $a9910713762303321 996 $aAerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10? to 11.0 x 10?$93500687 997 $aUNINA