02074oam 2200517I 450 991071388260332120200825082824.0(CKB)5470000002504865(OCoLC)1100474478(EXLCZ)99547000000250486520190508d1955 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds /by Bernard N. Daley and Douglas R. LordWashington, [D.C.] :National Advisory Committee for Aeronautics,1955.1 online resource (57 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3424"May 1955.""Supersedes recently declassified NACA RM L9E19. 1949"--Page 1.No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 10).Aerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speedsAerofoilsTestingAngle of attack (Aerodynamics)AerofoilsTestingfastAngle of attack (Aerodynamics)fastAerofoilsTesting.Angle of attack (Aerodynamics)AerofoilsTesting.Angle of attack (Aerodynamics)Daley Bernard N.1404413Lord Douglas T.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713882603321Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds3478941UNINA