02142oam 2200589 450 991071686300332120210924140653.0(CKB)5470000002525555(OCoLC)1159597683(EXLCZ)99547000000252555520200623d1938 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps /by Carl J. Wenzinger and Milton B. Ames, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1938.1 online resource (11 pages, 9 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 661"August 1938."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 10).AirplanesWingsTestingSplit flaps (Airplanes)AileronsWind tunnel testingAileronsfastAirplanesWingsTestingfastSplit flaps (Airplanes)fastWind tunnel testingfastAirplanesWingsTesting.Split flaps (Airplanes)Ailerons.Wind tunnel testing.Ailerons.AirplanesWingsTesting.Split flaps (Airplanes)Wind tunnel testing.Wenzinger Carl J(Carl Joseph),1903-1988,1386955Ames Milton B.Jr.,United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910716863003321Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps3469422UNINA