02531oam 2200697I 450 991071376230332120200729144450.0(CKB)5470000002504060(OCoLC)1100474481(EXLCZ)99547000000250406020190508d1949 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶ /by Raymond F. Schaefer and Hamilton A. SmithWashington, [D.C.] :National Advisory Committee for Aeronautics,1949.1 online resource (12 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 1998"December 1949."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 8).Aerodynamic 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)AerofoilsAerodynamicsLift (Aerodynamics)Drag (Aerodynamics)Pitching (Aerodynamics)Wind tunnel testingAerodynamicsfastAerofoilsfastDrag (Aerodynamics)fastLift (Aerodynamics)fastPitching (Aerodynamics)fastWind tunnel testingfastAerofoils.Aerodynamics.Lift (Aerodynamics)Drag (Aerodynamics)Pitching (Aerodynamics)Wind tunnel testing.Aerodynamics.Aerofoils.Drag (Aerodynamics)Lift (Aerodynamics)Pitching (Aerodynamics)Wind tunnel testing.Schaefer Raymond F.1410898Smith Hamilton A.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713762303321Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10⁶ to 11.0 x 10⁶3500687UNINA