01644oam 2200469 450 991071534610332120210226094833.0(CKB)5470000002510574(OCoLC)1145759599(EXLCZ)99547000000251057420200323d1934 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierTests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections /by Raymond F. AndersonWashington, [D.C.] :National Advisory Committee for Aeronautics,1934.1 online resource (8 pages, 5 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 487"January 1934."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).AerofoilsWind tunnel testingAerodynamicsAerodynamicsfastAerofoils.Wind tunnel testing.Aerodynamics.Aerodynamics.Anderson Raymond F.91081United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910715346103321Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections3522095UNINA